PROGRAMA DE MANTENIMIENTO AVIONES EMB - 145

05/Abril/2010

PUBLICADO POR:

Aerolitoral S.A. de C.V. Carretera Miguel Alemán Km. 22.8 Apodaca, N.L. C.P. 66600, México Tel . (81) 82-21-16-00 Fax. (81) 82-21-16-30

EMB-145 Maintenance Program Programa de Mantenimiento EMB-145 CARTA DE REVISIÓN

Code: M-PME-01 Revision: 2 Fecha de Efectividad: 05-Abr-10 Page: 1

Carta de Revisión

A: Todos los responsables del Programa de Mantenimiento EMB-145.

Revisión 2, 05-Abr-10

Resumen

Se emite la presente modificación debido a: Actualización del manual MRB Revisión 14. Se eliminan las secciones de tareas independientes. Se elimina la sección de formatos internos.

. Para actualizar el manual: Sustituya el CD Manual de Programa de Mantenimiento PME-145 de fecha 20-Sep-09 con el CD de fecha 05-Abr-2010.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program INTRODUCCION

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. i

ÍNDICE

Índice Registro de Revisiones Registro de Revisiones temporales Lista de Paginas Efectivas

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SECCIÓN 1. DESCRIPCIÓN DEL PROGRAMA 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8

General Limites de Tiempo Descripción General del Programa Definición de Servicios Cambio de los Intervalos de Inspección/Mantenimiento. Programa de los Motores y APU Definición de Términos Abreviaturas y Acrónimos

1-1-1 1-2-1 1-3-1 1-4-1 1-5-1 1-6-1 1-7-1 1-8-1

SECCIÓN 2. REQUERIMIENTOS DE INSPECCIÓN DE SERVICIOS MENORES SECCIÓN 3. REQUERIMIENTOS DE INSPECCIÓN DE SISTEMAS Y PLANTA MOTRIZ SECCIÓN 4. REQUERIMIENTOS DE INSPECCIÓNES ESTRUCTURALES SECCIÓN 5. PROGRAMA DE PREVENCIÓN Y CONTROL DE LA CORROSION (CPCP) SECCIÓN 6. REQUERIMIENTOS DE INSPECCIÓN POR ZONAS SECCIÓN 7. REQUERIMIENTOS DE MANTENIMIENTO POR CERTIFICACIÓN (CMR’S) SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA SECCIÓN 9. REQUERIMIENTOS DE MANTENIMIENTO CATEGORIA II SECCIÓN 10. REDUCCION DEL LIMITE DE SEPARACION VERTICAL (RVSM) SECCIÓN 11. LIMITACIONES DEL SISTEMA DE COMBUSTIBLE SECCIÓN 12. TAREAS RECOMENDADAS SECCIÓN 13. TAREAS DE COMPONENTES REEMPLAZO MANTENIMIENTO LINEA. SECCIÓN 14. TAREAS DE COMPONENTES REEMPLAZO MANTENIMIENTO MAYOR. SECCIÓN 15. TAREAS NO APLICABLES SECCIÓN 16. FORMATOS INTERNOS

REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program INTRODUCCION

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. ii

REGISTRO DE REVISIONES Mantenga este registro en el Manual. Al recibir las revisiones, remueva e inserte las páginas revisadas del Manual y posteriormente anote la fecha de la revisión, la fecha de inserción y sus iniciales. Revisión No.: Original 1 2

Fecha de Revisión: 24/07/09

Fecha de Inserción: 15/08/09

Insertado Por: RMR

20/09/09

5/11/09

RMR

05/04/10

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Atención usuarios: Favor de conservar su registro de revisiones, esta hoja es solo de referencia.

REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program INTRODUCCION

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. iii

REGISTRO DE REVISIONES TEMPORALES Mantenga este registro en el Manual. Al recibir las revisiones temporales, inserte las páginas revisadas en el Manual y posteriormente anote la fecha de la revisión, la fecha de inserción y sus iniciales. Revisión No

Fecha de Revisión:

Fecha de Inserción:

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REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program INTRODUCCION

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. iv

LISTA DE PAGINAS EFECTIVAS

INTRODUCCIÓN Índice Registro de Revisiones Registro de Revisiones Temporales Lista de Paginas Efectivas

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SECCIÓN 1. DESCRIPCIÓN DEL PROGRAMA

1.1 General

1.2 Limites de Tiempo 1.3 Descripción General del Programa

1.4 Definición de Servicios

1.5 Cambio de los Intervalos de Inspección / Mantenimiento. 1.6 Programa de los Motores y APU 1.7 Definición de Términos REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program INTRODUCCION

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. v

1.8 Abreviaturas y Acrónimos

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SECCIÓN 2. REQUERIMIENTOS DE INSPECCIÓN RUTINARIOS

SECCIÓN 3. REQUERIMIENTOS DE INSPECCIÓN DE SISTEMAS Y PLANTA MOTRIZ

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURAL

REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program INTRODUCCION

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SECCIÓN 5. PROGRAMA DE PREVENCIÓN Y CONTROL DE LA CORROSION (CPCP)

SECCIÓN 6. REQUERIMIENTOS DE INSPECCIÓN POR ZONAS

SECCIÓN 7. REQUERIMIENTOS DE MANTENIMIENTO POR CERTIFICACIÓN (CMR’S)

SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA

REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program INTRODUCCION

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. vii

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SECCIÓN 9. REQUERIMIENTOS DE MANTENIMIENTO CATEGORIA II

SECCIÓN 10. REDUCCION DEL LIMITE DE SEPARACION VERTICAL (RVSM) SECCIÓN 11. LIMITACIONES DEL SISTEMA DE COMBUSTIBLE

SECCIÓN 12. TAREAS RECOMENDADAS

SECCIÓN 13. TAREAS DE COMPONENTES REEMPLAZO MANTENIMIENTO LINEA

SECCIÓN 14. TAREAS DE COMPONENTES REEMPLAZO MANTENIMIENTO MAYOR SECCIÓN 15. TAREAS NO APLICABLES

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Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program INTRODUCCION

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. viii

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SECCION 16. TAREAS INTERNAS JC256007ALE JC237001ALE

JC282101ALE

34-61-00-470-801-A (Tarea AMM) 34-62-00-400-801-A (Tarea AMM) 34-62-00-400-802-A (Tarea AMM)

REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-1-1

1.1 GENERAL El Programa de Mantenimiento del Embraer EMB-145 contiene tareas de mantenimiento programado que aseguran la continuidad de la aeronavegabilidad del fuselaje del EMB-145, así como de sus motores y componentes. El Programa de Mantenimiento del Embraer EMB-145, a partir de aquí referido como el Mantenimiento es aplicable a la flota de EMB-145 de Aerolitoral. El Programa de Mantenimiento está basado en el Maintenance Review Board Report (MRBR) Revisión 14. El presente programa además de contener las tareas requeridas por el fabricante, también contiene aquellas tareas generadas por la experiencia de la operación de Aerolitoral, resultado de modificaciones derivadas de la incorporación de STCs, y/o Boletines de Servicio, tareas que han sido desarrolladas por el Departamento de Ingeniería de Aerolitoral para mejorar el mantenimiento de la aeronave y la flota en su conjunto, dichas tareas se incorporan dentro de la sección 16 “Tareas Internas” del Programa de Mantenimiento. Su nomenclatura que las denomina es un número de 8 caracteres de la manera siguiente: ¾ ¾ ¾ ¾

Los primeros dos dígitos son del capítulo ATA. El tercer y cuarto dígitos indican el subcapitulo ATA. El quinto y sexto dígitos indican un numero consecutivo Al final se agregan las siglas ALE que indican que la tarea fue desarrollada por Aerolitoral para el equipo Embraer 145.

Las tareas (TASK’s) que componen el programa de mantenimiento, deben efectuarse a determinados intervalos: Horas de Vuelo (Flight Hours – FH) Aterrizajes (Flight Landings / FL), Ciclos (Flight Cycles – FC) o tiempos Calendario. Los tiempos calendario son: Días (D) Meses (Months - MOS) o Años (Years - YR). Nota: Con el fin de tener un programa de mantenimiento flexible para la aplicación de tareas, en este programa, todas las tareas se manejaran como tareas independientes, con lo cual no se tendrá la rigidez de manejar estas dentro de formatos.

Para el caso de los APU’s, se considera que un FC, es cada vez que se lleva a cabo un evento de operación del APU, (arranque, operación, corte). Este Programa de Mantenimiento está dividido en las siguientes secciones, y están incluidas en el Programa de Mantenimiento de acuerdo con las políticas y procedimientos de Aerolitoral.

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Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-1-2

Sección 1. Descripción del Programa Sección 2. Requerimientos de Inspección de Servicio Menores Sección 3. Requerimientos de Inspección de Sistemas y Planta Motriz Sección 4. Requerimientos de Inspecciones Estructurales Sección 5. Programa de Prevención y Control de la Corrosión (CPCP) Sección 6. Requerimientos de Inspección por Zonas Sección 7. Requerimientos de Mantenimiento por Certificación (CMRs) Sección 8. Componentes Limitados por Vida Sección 9. Requerimientos de Mantenimiento Categoría II Sección 10. Reducción del límite de separación vertical (RVSM) Sección 11. Limitaciones del Sistema de Combustible Sección 12. Tareas Recomendadas Sección 13. Tareas de Componentes Reemplazo Mantenimiento Linea. Sección 14. Tareas de Componentes Reemplazo Mantenimiento Mayor. Sección 15. Tareas No Aplicables Sección 16. Formatos Internos (Tareas Internas) Este documento proporciona una lista de páginas efectivas como un medio de mantener y actualizar el Programa de Mantenimiento. Al recibir alguna revisión del documento, esta lista debe ser utilizada como una referencia cruzada para insertar los nuevos datos. Los datos obsoletos serán destruidos y el Programa de Mantenimiento se mantendrá actualizado todo el tiempo. Cada página revisada contendrá la fecha de la revisión y la línea identificadora de la revisión, en el margen izquierdo de la página, la cual identificará adiciones, remociones o cambios a los datos. Sin importar el tipo de medio ambiente de operación, las limitaciones que están descritas y especificadas en este Manual, serán aplicables a los aviones Embraer EMB-145. Aerolitoral proporcionará un programa de mantenimiento comprensible, necesario para cumplir con su responsabilidad de mantener sus aviones en una condición aeronavegable, de acuerdo con la normatividad de la Dirección General de Aeronáutica Civil (DGAC). El avión, sus componentes y accesorios deben ser mantenidos en una condición aeronavegable de acuerdo con los límites máximos de tiempo como se autoriza en este documento. APLICABILIDAD El contenido de este documento es aplicable para las aeronaves EMBRAER: EMB-145 LR EMB-145 MP EMB-145 EP REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-1-3

EMB-145 LU Sin embargo, con las revisiones adecuadas, puede ser ampliado para los siguientes modelos: EMB-145 ER/EU/MR/MK/XR Las Tareas de mantenimiento que únicamente sean aplicables a algunos modelos o a toda la flota se reflejara dentro de la columna de efectividad. REGLAS GENERALES 1. El programa de mantenimiento debe ser efectuado de acuerdo con los Manuales Técnicos editados para las aeronaves Embraer EMB-145, tales como el Manual de Mantenimiento del avión y/o tarjetas de trabajos específicas. (Ref. Manual General de Mantenimiento y Procedimientos de Taller) 2. En cualquier lugar del avión donde se efectúe una tarea programada, la estructura, sistemas y área adyacente al área afectada tendrán que ser revisadas por condición y daños antes de dejar el área. 3. Las Tareas calificadas como Requerimientos de Mantenimiento por Certificación (CMRs) y los Componentes Limitados por tiempo se encuentran descritos en la Secciones 7 y 8 respectivamente en este Documento. Estos límites pueden ser revisados y aplicados de manera inmediata de acuerdo con las recomendaciones del fabricante, mismos que se actualizaran en la siguiente Revisión Formal del Programa de Mantenimiento Embraer EMB 145 ante la Dirección General de Aeronáutica Civil (DGAC). 4. Las frecuencias de las tareas de mantenimiento que se muestran en este documento pueden ser modificadas de acuerdo a lo establecido en el manual MRBR vigente. 5. En este documento los términos “Check” e “Inspection” no implican un grado de habilidad para realizar la tarea. El Manual General de Mantenimiento y de Procedimientos de Taller aprobado por Aerolitoral describe los requerimientos para que el personal pueda efectuar una tarea. 6. Aerolitoral puede tomar créditos de Tareas descritas en este documento,

cuando se realicen por la tripulación de vuelo. Dichas tareas pueden ser incluidas en las listas de verificación revisadas y aprobadas por la DGAC, ó en el Manual de Técnica de Vuelo aprobado del EMB-145. 7. Cuando existan cambios en el contenido del Programa de Mantenimiento por parte del fabricante, derivados de actualizaciones temporales; cambios en los REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-1-4

limites de vida de los componentes y/o directivas de aeronavegabilidad por parte de las autoridades regulatorias, de características tales, que no sea práctico publicar como parte del contenido de una Revisión Formal, por el tiempo que implica tramitar la autorización oficial así como su impresión y publicación , se emitirán revisiones temporales. Dichas revisiones Temporales no requerirán autorización expresa de la Dirección General de Aeronáutica Civil (DGAC). Toda revisión temporal deberá ser identificada con el texto “Revisión Temporal” e impresa en hojas de color amarillo. Toda información que sea considerada urgente será distribuida vía Fax o Correo electrónico interno, en tanto los poseedores de los manuales reciben la revisión temporal impresa. Las revisiones temporales (amarillas) al PME se emitirán de forma consecutiva (Rev. Temp.1, Rev. Temp.2, Rev. Temp.3, etc.) Re-inicializando el consecutivo (Rev. Temp.1, Rev. Temp.2, Rev. Temp.3, etc.) por cada Revisión Formal (blanca) publicada.

8. Los capítulos están numerados en forma progresiva, al igual que las secciones y las páginas de cada capítulo, como se muestra a continuación. página

2–2-1 | | |__________ | |_____________ |________________

Página Sección Capitulo

9. Cuando sea posible de agrupar más de una tarea para efectuar en un mismo evento, que sean del mismo intervalo ó que convenga a la empresa, se podrá hacer uso de la platilla a fin de reducir el manejo de papelería. Nota: De forma indistinta la existencia del uso de la plantilla para la agrupación de tareas por parte de Aeromexico Connect, no significa que se puedan incrementar los intervalos individuales de las tareas, por el contrario la empresa continuara respetando los limites indicados en cada una de las tareas como hasta ahora.

10. Para el caso de las tareas independientes se mandara a la realización usando la forma F-GIN-01 Orden de Trabajo (ver MGM y PT capitulo 13).

REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-1-5

REV. 01

No.

Titulo de casilla

Debe anotarse

Generador

1

Code

El código propuesto

2

Revisión

3

Intervalo

La revisión de acuerdo a la revisión del M-PME-145 El intervalo común de las tareas

4

Fecha de efectividad

5

Pagina

La fecha de acuerdo a la revisión del M-PME-145 Página “X” de “XX”

6 7 8

A/C registro Fecha Item

Matricula de la aeronave La fecha de inicio de las tareas Número consecutivo

9

Tarea

10

Tipo

11

Categoría

12

Descripción

Código de la tarea de acuerdo al MPME-145 y MRBR Tipo de tarea de acuerdo al M-PME145 (cuando aplique) Categoría de acuerdo al M-PME-145 (cuando aplique) La descripción de la tarea a efectuarse

13 14

Técnico Inspección

Ingeniería y/o planeación Ingeniería y/o planeación Ingeniería y/o planeación Ingeniería y/o planeación Ingeniería y/o planeación Mantenimiento Mantenimiento Ingeniería y/o planeación Ingeniería y/o planeación Ingeniería y/o planeación Ingeniería y/o planeación Ingeniería y/o planeación Mantenimiento Inspección

15

Nombre

16

Licencia número

17 18

Fecha Estación

19

Firma

Firma del técnico que efectuó el trabajo Firma del inspector que certifica el trabajo (cuando aplique) Nombre del técnico que esta cerrando y participo en los trabajos Número de licencia del técnico que cierra los trabajos Fecha de terminación del trabajo La estación donde se efectuaron los trabajos Firma del técnico que cierra los trabajos

Mantenimiento Mantenimiento Mantenimiento Mantenimiento Mantenimiento

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-1-6

REGLA DE FDR, CVR, COMPASS SWING Y ALTIMETROS Con el fin de realizar las tareas de calibración de Altímetros y Compas Swing, Aerolitoral en apego a las instrucciones de los fabricantes, ha establecido realizar estas tareas cada 24 meses. Para la lectura de la Grabadora de Datos de Vuelo (FDR) se ha establecido un intervalo de 5000FH. y para la Cockpit Voice Recorder (CVR) un intervalo de 12 Meses. INCORPORACION DE TAREAS El Programa de Mantenimiento de EMB-145 es continuamente afectado por las Revisiones al MRBR o documentos de las Autoridades, por lo que se generan Revisiones Formales al PME y/o a las Tarjetas de Trabajo (Job Cards). REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-1-7

Estas revisiones se realizan de acuerdo a un Proceso básico que comprende: ¾ Recepción del Documento de Revisión emitido por el fabricante o Autoridad. ¾ Análisis de aplicabilidad e incorporación de modificaciones al PME Aerolitoral. ¾ Edición del Documento PME y envío a la Autoridad para su aprobación. ¾ Recepción de la revisión autorizada por DGAC al PME. Las Revisiones al MRBR emitidas por el fabricante, serán incorporadas mediante el proceso antes descrito al PME de Aerolitoral, dicha actualización se realizara una vez al año. Las Revisiones Temporales al MRBR (Amarillas) emitidas por el fabricante, serán incorporadas conforme a las “Reglas Generales” antes descritas y a consideración de Aerolitoral para su incorporación en el PME. VIGENCIA Las revisiones al Programa de Mantenimiento del EMB-145 entrarán en vigor a los 90 días posteriores a su autorización por DGAC. Durante este periodo se procederá a la edición de los formatos a utilizar, su difusión y distribución, así como la incorporación de las tareas y servicios en el Sistema de Planeación y Control. Cumplido lo anterior se iniciará la aplicación de las tareas revisadas conforme a la revisión aprobada. FECHA EFECTIVA DE INCORPORACION DE TAREAS Y SERVICIOS REVISADOS EN SU UMBRAL DE INCORPORACION O INTERVALO REPETITIVO. A la fecha de entrada en vigor de la nueva revisión, las Tarea(s) Repetitiva(s) que hayan sido afectada(s) en el valor de su Intervalo Repetitivo o Umbral de Incorporación por una nueva revisión al PME y cuyo ajuste provoque una afectación en la Programación y Planeación del Mantenimiento, se mantendrá por única y última ocasión su intervalo y/o umbral de incorporación anterior. FECHA EFECTIVA DE INCORPORACION DE TAREAS Y SERVICIOS NUEVOS. Las Tareas o Servicios Nuevos de la revisión deberán cumplirse posterior a la fecha de entrada en vigor dentro del próximo servicio de 5000FH ó 5000 FC ó 30 meses, según el tipo de intervalo que aplique, o el tamaño del intervalo de la tarea a partir de la entrada en vigor, lo que ocurra después.

REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Código: M-PME-01

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program

Número de Revisión: 2 Fecha Efectividad: 05-Abr-10

SECCION 1. DESCRIPCION DEL PROGRAMA

Pág. 1-1-8

EJEMPLO: a) Si una Tarea Incluida en un Formato de Servicio Disminuye o Aumenta su Intervalo, se mantendrá por única y última ocasión su umbral y/o intervalo, para posteriormente dar cumplimiento con el nuevo intervalo. ¾ Tarea Revisada que modificó su intervalo de 1000FH a 800FH (

)

ENTRADA EN VIGOR MOMENTO DE INCORPORACION DE NUEVO INTERVALO

Proceso de Incorporación

Efectividad / Inicio PME

UMBRAL DE INCOPRPORACION Día 90 después de Autorizado

Día 1 Autorización

Intervalo de Servicio 1000FH Revisión previa

800FH Tarea Repet.

Intervalo de Servicio 1000FH Intervalo de Servicio 800FH Revisión previa Revisión Nueva

b) Si una Tarea o Servicio es Nuevo, iniciará su aplicación a partir de alcanzar su primer intervalo de tiempo ó próximo servicio de 5000FH, posterior a la entrada en vigor de la revisión al PMS (lo que ocurra después). ¾ Tarea Nueva con intervalo de 1500 FH (

)

ENTRADA EN VIGOR

MOMENTO DE INCORPORACION

Proceso de Incorporación

Efectividad / Inicio PME

Día 1 Autorización

UMBRAL DE INCOPRPORACION Día 90 después de Autorizado

1500FH Tarea Nueva

Aplicación de Servicio de 4000FH con Tarea Nueva

1500FH Intervalo entre servicio de 5000FH

REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-1-9

DIRECTIVAS DE AERONAVEGABILIDAD Y/O BOLETINES DE SERVICIO. Directivas de Aeonavegabilidad y/o Boletines de Servicio Mandatorios que requieran aplicación periódica o alguna acción terminal, y que estén relacionadas con alguna Tarea del Programa de Mantenimiento, serán incorporadas como notas en “letras negritas” en la descripción de la tarea para indicar que el cumplimiento de la Directiva de Aeronavegabilidad o Boletín se Servicio se efectúa con la tarea especificada. Lista de Directivas de Aeronavegabilidad que se cumplen periódicamente con tareas programadas de Programa de Mantenimiento PME de Aerolitoral.

TAREA DE MRB en PME Aerolitoral

DESCRIPCION

FAA AD

ANAC AD

74-08-09 R2 párrafo e)1 y e)2.

-

2005-13-22

2000-08-01 R2

25-40-01-220-001-A00

Waste Receptacles

28-21-01-220-001-A00

Inspect Electric Connector

72-63-01-710-001-A00

Operationally Check Starter Drain Adapter

99-02-51

-

72-63-10-700-801

Engine Oil from the Starter shaft seal

99-02-51

-

Ailerons PCA and Damper

99-05-04

99-02-01 R6

27-12-01-212-002-A05 27-12-01-212-002-A06

Fuel

Pump

72-21-01-200-801

Fan Wheel inspection

2000-11-22

-

79-34-00-212-001-A00

Inspect for bearing contamination of the Oil System

2004-04-05

-

78-34-01-720-001-A00

Functionally Check Stow/Transit Thrust Reverser Microswitches for insulation

2001-17-03 párrafo b)

2001-05-03R3

79-34-00-212-001-A00

JC272000ALE N/A toda la flota esta modificada. 53-12-00-250-801-A00

REV. 01

2004-13-16

Inspect Multi-Function Display for ENG 1(2) OIL DEBRIS Maintenance Message

2004-04-05 párrafo f)

-

Verify reports of vibration from the tail section or rudder pedals over the last two days

-

BAD 2005-0902R1

New MRB task covering SSI 5310-19 Pre-Mod SB145-53-0058 special detailed inspection, internal side, zone 223/224

2007-07-02

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-1-10

53-12-00-250-801-A01

New MRB task covering SSI 5310-19, post-mod SB145-53-0058, special detailed inspection, internal side zone 223/224

28-11-00-720-001-A00

Functionally Check critical bonding integrity of selected conduits inside the wing tank, Fuel pump and FQIS connectors at tank wall by conductivity measurements.

2008-13-14

2007-08-02

28-17-01-720-001-A00

Functionally Check critical bonding integrity of Fuel pump, VFQIS and Low Level SW connectors at tank wall by conductivity measurements.

2008-13-14

2007-08-02

28-21-01-220-001-A00

Inspect Electric Connector

2008-13-14

2007-08-02

28-23-03-220-001-A00

Inspect Pilot Valve inside the conduit

Harness

2008-13-14

2007-08-02

28-23-04-220-001-A00

Inspect Vent Valve inside the conduit

Harness

2008-13-14

2007-08-02

28-27-01-220-001-A00

Inspect Electric Fuel Transfer Pump Connector

2008-13-14

2007-08-02

28-41-01-720-001-A00

Functionally Check Conditioning (FCU)

2008-13-14

2007-08-02

28-41-03-220-001-A00

Inspect FQIS harness for clamp and wire jacket integrity

2008-13-14

2007-08-02

28-41-04-720-001-A00

Functionally Check Ventral Fuel conditioning Unit (FCU)

2008-13-14

2007-08-02

28-41-07-220-001-A00

Inspect VFQIS and Low Level SW Harness for clamp and wire jacket integrity

2008-13-14

2007-08-02

Fuel

Pump

Fuel

Tasks into sections 4, 5,

57-26-00-250-813-A00

REV. 01

2007-07-02

2009-01-05

Externally inspect the WING components using Eddy Current inspection method: • Aft upper Trunnion (SSI 57-26-95)

2009-05-02

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-1-11

57-26-00-250-813-A01

57-26-00-250-813-A02

57-26-00-250-813-A03

57-26-00-250-813-A04

57-26-00-250-813-A05

57-26-00-250-815-A00

57-26-00-250-815-A01

57-26-00-250-815-A02

REV. 01

Externally inspect the WING components using Eddy Current inspection method: • Aft upper Trunnion (SSI 57-26-95) Externally inspect the WING components using Eddy Current inspection method: • Aft upper Trunnion (SSI 57-26-95) Externally inspect the WING components using Eddy Current inspection method: • Aft upper Trunnion (SSI 57-26-95) Externally inspect the WING components using Eddy Current inspection method: • Aft upper Trunnion (SSI 57-26-95) Externally inspect the WING components using Eddy Current inspection method: • Aft upper Trunnion (SSI 57-26-95) Externally inspect the WING components using Eddy Current inspection method: • Aft upper Trunnion (SSI 57-26-95) NOTE: Applicable only to trunnion P/N 145-67014001/002/003/004/005/006/007/008. Externally inspect the WING components using Eddy Current Inspection Method: • Aft upper Trunnion (SSI 57-26-95) NOTE: Applicable only to trunnion P/N 145-67014-011/012. Externally inspect the WING components using Eddy Current Inspection Method: • Aft upper Trunnion (SSI 57-26-95) NOTE: Applicable only to trunnion P/N 145-67014-009/010/013/014.

2009-05-02

2009-05-02

2009-05-02

2009-05-02

2009-05-02

2009-05-02

2009-05-02

2009-05-02

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-1-12

57-10-00-250-801-A00

28-41-01-720-001-A01

REV. 01

Externally inspect the WING STUB components using Eddy Current inspection method: • Rib 4 – lower flange and web (SSI 57-10-11) NOTE: Applicable to aircraft PreMod. SB 145-57-0047.

. Functionally Check Fuel Conditioning (FCU)

2009-05-02

2009-08-03

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-2-1

1.2 LIMITES DE TIEMPO

INTERVALOS DEL PROGRAMA DE MANTENIMIENTO Los intervalos para la aplicación de las tareas de mantenimiento programados se efectúan en base a codificaciones de letras y/o números que determinan el tiempo e intervalos para aplicar las tareas de mantenimiento requeridas en las aeronaves. Las siguientes letras están designadas por el fabricante (código de intervalo) Embraer y que indican los siguientes intervalos a las tareas del programa de mantenimiento de las aeronaves Embraer EMB-145: Servicio “A” = 500 FH Servicio “C” = 5000 FH, 5000 FC ó 2.5 años Para los múltiplos de “A”, los intervalos básicos son multiplicados por el número próximo a la letra y serán utilizados hasta 5A (P.E. 2A=1,000 FH, 5A=2500 FH, etc.). Para los múltiplos de “C”, los intervalos básicos son multiplicados por el número próximo a la letra y serán utilizados hasta 2C (P.E. C1=5000 FH, 5000 FC ó 30 Meses (lo que ocurra primero); 2C=10,000 FH, 10,000 FC ó 60 Meses (lo que ocurra primero) y 4C=20,000 FH, 20,000 FC ó 120 Meses (lo que ocurra primero). Así mismo, considerando que todas las tareas dentro de este programa se realizaran de forma independiente como se ha mencionado en la pagina 1-1-1, y que al igual podrán ser agrupadas dentro de una plantilla como se menciona en la pagina 1-1-4, con el fin de buscar una rápida alineación de las tareas que pueden ser agrupadas Aeromexico Connect, basados en su experiencia, determino las identificaciones listadas en la tabla 1. Lo anterior no significa que la empresa no pueda alinear mas tareas, con alguna otra designación de código Para las tareas denominadas “Prior to Winter” (PW) el intervalo anual se aplicará en los meses de Octubre, Noviembre, Diciembre ó Enero dependiendo de la planeación de las aeronaves para su mantenimiento y será a criterio del departamento de Planeación y Control.

REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-2-2

TABLA 1 LISTA DE CÓDIGOS PARA AGRUPACIÓN DE TAREAS A continuación se presenta un listado de los códigos a usarse de forma común, para la agrupación de las tareas del Mantenimiento de las aeronaves EMBRAER ERJ-145. CÓDIGO F-PME-01 F-PME-03 F-PME-04 F-PME-06 F-PME-07 F-PME-11 F-PME-12 F-PME-15 F-PME-17 F-PME-18 F-PME-21 F-PME-21 F-PME-21 F-PME-21 F-PME-30 F-PME-31 F-PME-41 F-PME-46 F-PME-47 F-PME-51 F-PME-51 F-PME-51 F-PME-61 F-PME-64

REV. 01

DESCRIPCIÓN Servicio de 48 HOURS LC1 (10 DAYS) LC2 (40 DAYS) 4000 FH 8000 FH A (500 FH) 2A (1000 FH) 5A (2500 FH) E (2500 FC) E (2500 FC) EMPENAJE C1 (SYSTEMS) 1 DE 4 C1 (ZONAL) 2 DE 4 C1 (ESTRUCTURAL) 3 DE 4 C1 (CORROSION PROGRAM) 3 DE 4 E (48 MOS + C1) E (72 MOS + C1) C2 (SYSTEMS) E (20000 FC + C2) E (96 MONTHS + C2) C4 (SYSTEMS) 1 DE 3 C4 (ZONAL) 2 DE 3 C4 (STRUCTURAL) 3 DE 3 E (30000 FC) PRIOR TO WINTER

FECHA DE REVISIÓN 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10 05-Abr-10

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-3-1

1.3 DESCRIPCIÓN GENERAL DEL PROGRAMA REQUERIMIENTOS DE INSPECCION DE SERVICIOS MENORES (Sección 2) Esta sección contiene todos los requerimientos de Inspección de servicios menores de los sistemas y de la planta motriz resultantes del análisis MSG-3. Las inspecciones aquí establecidas son un conjunto de tareas rutinarias que cubren servicios y revisiones visuales de todo el avión por condición general. El método para determinar el programa de mantenimiento para los sistemas y la planta motriz es usando el protocolo MSG-3, el cual usa diagramas lógicos progresivos que son aplicados a los Componentes de Mantenimiento Significante (Maintenance Significant Items - MSI´s) del avión. Las tareas denominadas con las letra REC son tareas recomendadas, sin embargo Aerolitoral ha decidido incorporarlas en este programa para reducir posibles riesgos económicos derivados de fallas, por lo tanto pueden ser escaladas ó eliminadas bajo un fundamento estadístico y análisis pertinente en común acuerdo con la DGAC. Los MSI´s son aquellos componentes identificados por Embraer cuya falla: I. II.

Podría afectar la seguridad (en tierra o en vuelo), y/o Podría ser indetectable o no fácilmente detectable durante la operación, y/o III. Podría tener un significante impacto operacional, y/o IV. Podría tener un significante impacto económico.

Cada tarea tiene una categoría de clasificación que sigue la lógica MSG-3 para el efecto de la falla del componente significante de mantenimiento (MSI). CATEGORIA 5 6 7 8 9 REC

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CLASIFICACION DE TAREA Falla evidente – Impacto en la seguridad Falla evidente – Impacto en la operación Falla evidente– Impacto económico Falla oculta – Impacto en la seguridad Falla oculta – No impacto en la seguridad Tareas recomendadas - No impacto en la seguridad

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-3-2

REQUERIMIENTOS DE INSPECCION DE SISTEMAS Y PLANTA MOTRIZ (Sección 3) Los objetivos del programa de mantenimiento de los sistemas y planta motriz son: I.

Asegurar el nivel de seguridad y confiabilidad inherentes del equipo.

II.

Restaurar la seguridad y confiabilidad a su nivel inherente cuando ha ocurrido un deterioro.

III.

Obtener la información necesaria para mejorar el diseño de aquellos componentes cuya confiabilidad inherente se prueba inadecuada.

IV.

Realizar estos objetivos a un costo total mínimo, incluyendo costos de mantenimiento y el costo de falla residual.

Esta sección define las tareas de mantenimiento para los sistemas y la planta motriz, así mismo la sección, esta organizada de acuerdo al código ATA y la cual cubre los siguientes sistemas del avión: 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 38 45 49 52 53 71 72 REV. 01

Standard practices - airframe Aire Acondicionado y Presurización Vuelo Automático Comunicación Eléctrico Equipo Interior Protección contra Fuego Controles de Vuelo Combustible Hidráulico Protección contra Hielo y Lluvia Sistemas Indicadores / Grabadores de Datos Tren de Aterrizaje y Frenos Luces Navegación Oxigeno Neumático Agua Potable y Aguas Negras Sistema Central de Mantenimiento Potencia Auxiliar Puertas Fuselaje Planta Motriz Motor

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-3-3

73 74 76 78 79 80

Combustible del Motor Ignición del Motor Control del Motor Escape del Motor Aceite del Motor Arranque del Motor

Las tareas identificadas con categoría 5 y 8 no pueden ser omitidas, excepto con la aprobación conjunta de Embraer y la DGAC.

REQUERIMIENTOS DE INSPECCIONES ESTRUCTURALES (Sección 4) Esta sección contiene todos los requerimientos de inspección estructural resultantes del análisis MSG-3. Estos requerimientos consisten de tareas de mantenimiento e intervalos asociados desarrollados de acuerdo a la capacidad de operación certificada del avión, y tienen la intención de detectar y prevenir cualquier degradación estructural causada por fatiga, deterioro por medio ambiente o daños accidentales durante la vida operacional del avión. La detección de daños accidentales mayores tales como los causados por impactos de aves y equipo de tierra se considera obvia. El Ingeniero a cargo dará un “Reporte de Daños Estructurales” por el medio que crea conveniente (fax, telefono, correos electronicos, etc.) de acuerdo a lo marcado en la SNL 145-00-0065 Esta sección cubre los siguientes sistemas del avión: 32 52 53 54 55 57

Tren de Aterrizaje Puertas Fuselaje Pilones Estabilizador Ala

PROGRAMA DE PREVENCIÓN Y CONTROL DE LA CORROSION “CPCP” (Sección 5) Esta sección contiene los requerimientos de inspección para la prevención de la corrosión resultantes del análisis MSG-3. Estos requerimientos consisten de tareas de mantenimiento e intervalos asociados desarrollados para prevenir cualquier degradación estructural causada por deterioro del medio ambiente REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-3-4

durante la vida operacional del avión. Aerolitoral mantendrá en el Departamento de Inspección de Control de Calidad un registro de toda la detección y tratamiento de la corrosión en la flota de EMB-145. Toda la corrosión Nivel 2 y Nivel 3 que sea detectada será reportada a Embraer por el Ingeniero a cargo ” por el medio que crea conveniente (fax, teléfono, correos electrónicos, etc.), siempre y cuando existan daños detectados y reportados por los Inspectores de Control de Calidad a través del formato de “Registro de Daños y Reparación Estructural en Aeroplano” (F-GAC-42). El Programa de Prevención y Control de la Corrosión (CPCP) especificado en este programa es el punto de arranque del control de la corrosión, e implica que el Compuesto Inhibidor de la Corrosión (CIC) esté todavía aplicado, y que el control de aplicaciones subsecuentes de CIC debe ser iniciado a partir de la fecha de manufactura del avión. Los requerimientos básicos de la implementación de las Tareas de CPCP se encuentran descritas en el MRBR Sección 5, y deben ser seguidas para realizar los ajustes necesarios al programa, junto con lo especificado en el Manual de Prevención de la Corrosión de la aeronave EMB145. Una forma práctica para definir los niveles de corrosión detectados puede ser considerando el siguiente proceso:

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Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-3-5

Diagrama de Niveles de Corrosión Se detecta corrosión en un “Structural Significant Item” (SSI)/ Corrosion detected on a SSI (Structural Significant Item)

CORROSION NIVEL 1

NO

Es atribuido a un evento No Típico?/ Is attributed to an event no typical?

NO

La corrosión excede mas allá de los límites permisibles?/ Is corrosion blend out beyond allowable limits?

Es corrosión extendida? Is widespread corrosion?

NO

SI NO

SI

Es corrosión reparada muy cerca de los límites permisibles de retrabajo? Is single blend-out; Approaching; Allowable Rework limits?

CORROSION NIVEL 1

Es un daño potencial que afecta urgentemente a la aeronavegabilidad de la flota?/ Is the damage a potential urgent airworthiness concern in the operator fleet? NO

SI

SI

El Fabricante confirma que es un daño potencial que afecta la aeronavegabilidad? Does manufacturer confirm damage is a potential urgent airworthiness concern?

NO

CORROSION NIVEL 2

SI

CORROSION NIVEL 3

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Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-3-6

REQUERIMIENTOS DE INSPECCION POR ZONAS (Sección 6) Esta sección contiene los requerimientos de inspección por zonas resultantes del análisis MSG-3. Estos requerimientos consisten en series de Inspecciones Visuales Generales (GVI) desarrollados para cada zona del avión. Estas Inspecciones tienen la intención de revisar la instalación de sistemas del avión y los motores, así como la estructura del avión por seguridad y condición general. Criterios de la Inspección por Zonas Las Inspecciones Visuales Generales (GVI) deben ser efectuadas a la distancia del alcance de las manos, y puede ser utilizado un espejo para un mejor acceso visual a las superficies de las áreas inspeccionadas, a menos que se establezca otra cosa. Las GVI abarcan lo siguiente: • Examen de componentes por montaje correcto o sujeción a su soporte relacionado o equipo adyacente, por seguridad, abrazaderas flojas, juego excesivo, desalineamiento, tubería, mangueras o conexiones eléctricas flojas y remaches, pernos o tornillos perdidos. • Inspección de partes estructurales, tales como estructuras, mamparos, herrajes, largueros, refuerzos y soportes por remaches flojos, melladuras, abolladuras, roturas, separación de adhesivo, corrosión, limpieza erosión, deformación, combadura, tratamiento protector deteriorado y sobrecalentamiento. • Inspección de ductos, mangueras y componentes de sistemas de tuberías (tales como hidráulicas, combustible, aire acondicionado, pitot-estático, oxigeno, etc.) por melladuras, abolladuras, limpieza, roturas, rozamiento, fuga, distorsión, desgaste, corrosión, obstrucción, cortadas o sobrecalentamiento. • Inspección de cableado de sistemas eléctricos y electrónicos por erosión, pobre aislamiento, cortadas, deformación, pobre limpieza, rozamiento, sobrecalentamiento, soldadura defectuosa, incluyendo aquellos componentes como cables y conectores flojos. • Inspección de partes o áreas hechas de materiales compuestos, plástico, tela, , etc. por delaminación, rayones, limpieza, roturas, rozamiento, grietas, deterioro, erosión, desgaste, distorsión, protección defectuosa, descascaramiento, perdida de flexibilidad, sobrecalentamiento y contaminación.

REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-3-7

• Inspección de partes de mecanismos de control de vuelo por alineación, distorsión, pandeo, limpieza, cortaduras, goteras, rozamiento, deshilachamiento o desgaste de cables de control, roturas, separación de adhesivo, y corrosión.

REQUERIMIENTOS DE MANTENIMIENTO POR CERTIFICACION “CMR’S” (Sección 7) Esta sección contiene los requerimientos de mantenimiento por certificación que resultaron de los procedimientos de la AC 25-19 y establecidos por el Comité de Coordinación de Certificación de Mantenimiento (CMCC). Estas CMR´s son inspecciones establecidas a través del proceso de análisis de la seguridad desarrollado de acuerdo con las normas RBHA/FAR/JAR 25.1309, enfocándose en detectar fallas latentes que afecten significativamente la seguridad, y las que podrían en combinación con otra falla o evento mas especifico, resultar en una condición peligrosa de falla. Los CMR´s están referenciados en el Certificado Tipo del avión, son mandatorios y no pueden ser cambiados, ampliado su intervalo de inspección, o borrados sin la aprobación de Embraer.. Las Tareas calificadas como Requerimientos de Mantenimiento por Certificación (CMRs) cuyos límites sean revisados de acuerdo con las recomendaciones del fabricante pueden ser aplicados de manera inmediata por Aerolitoral, mismos que se actualizaran en la siguiente Revisión Formal del Programa de Mantenimiento Embraer EMB 145 ante la Dirección General de Aeronáutica Civil (DGAC).

COMPONENTES LIMITADOS POR VIDA (Sección 8) Esta sección contiene las tareas de Componentes Limitados por Vida en el MRBR sus limites o intervalos no pueden ser cambiados o borrados sin la aprobación de Embraer. Las Tareas calificadas como Componentes Limitados por tiempo cuyos límites sean revisados de acuerdo con las recomendaciones del fabricante pueden ser aplicados de manera inmediata por Aerolitoral de acuerdo con las recomendaciones del fabricante, mismos que se actualizaran en la siguiente Revisión Formal del Programa de Mantenimiento Embraer EMB 145 ante la Dirección General de Aeronáutica Civil (DGAC).

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Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-3-8

REQUERIMIENTOS DE MANTENIMIENTO CATEGORIA II (Sección 9) Esta sección contiene las tareas de mantenimiento necesarias para cumplir con los requerimientos de rendimiento para la operación CAT II descrita en la AC-12029. El cumplimiento de estas tareas iniciará una vez autorizada y certificada la operación CAT II. REDUCCION DEL LIMITE DE SEPARACIÓN VERTICAL “RVSM” (Sección 10) Esta sección contiene las tareas de mantenimiento adicionales y necesarias para asegurar el nivel de rendimiento y confiabilidad de los sistemas relacionados, para cumplir con los requerimientos para la operación en la reducción del límite de separación mínima vertical. El cumplimiento de estas tareas iniciará una vez autorizada y certificada la operación RVSM. LIMITACIONES DEL SISTEMA DE COMBUSTIBLE (Sección 11) Estas limitaciones son mandatarias derivadas del tanque de combustible de una fuente de valoración de seguridad y el cumplimiento de los requerimientos de RBHAE 88, SFAR 88 y el memorando ANM112-05-011 de la FAA, política de declaración en proceso para el desarrollado SFAR No. 88 instrucciones relativas para el mantenimiento e inspección del tanque de combustible y la política de declaración EASA en los procesos por instrucciones reveladas por mantenimiento e inspección de la fuente preventiva del sistema del tanque de combustible Estas limitaciones son para mantener los requerimientos de la seguridad de fallas futuras y excluir la existencia o desarrollo de fuentes de ignición en el sistema del tanque de combustible durante toda la vida operacional de la aeronave. Aerolitoral aplicara la implementación de las limitaciones de combustible de acuerdo con la revisión 10 del MRB sección A2-66. La primer inspección mandatoria será cumplida en el próximo servicio C o en cada intervalo de inspección, contenida en cada punto de la sección 11, lo que ocurra ultimotas tarde. CONTROL DE LIMITACIONES EN LA CONFIGURACION CRÍTICA DEL DISEÑO Critical Design Configuration Control Limitation (CDCCL) CDCCL son las características en el diseño, de aeronaves, las cuales se utilizan para prevenir y prever fuentes de ignición en el sistema de combustible. REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-3-9

Siendo la razón para remarcar estas características de diseño, como CDCCL´s es alertar que las acciones de mantenimiento o cambios de configuración no deben mostrar ninguna afectación en las características de diseño originales Basados en los requerimientos de SFAR88 las siguientes características son consideradas como CDCCL ´s: 1. Arneses de los tanques de combustible en las alas FQIS/HLEIS con arneses FCU/LCU con conectores de pared del mismo tanque de combustible. Estos arneses corren desde los tanques del ala FCU y LCU, por debajo del piso, de la cabina de pilotos, pasando a través de un conector de interfase del STUB SPAR #1 (pressurized cabin to the fairing), divididos en 2, encontrándose el conector en la pared de un tanque hermético en cada ala Este arnés esta identificado y remarcado como CDCCL en los procedimientos de AMM para mantener la correcta instalación, sin permitir alteraciones que puedan violar la configuración del diseño del fuel Quanity Indicating System y del Higt Level Exceeding Indication System (si este es aplicable) del arnés exterior del tanque de combustible. Esta comprobación debe cumplirse cada vez que se realiza una tarea de mantenimiento, o en cualquier área cercana que pueda afectar la instalación de arnés. 2. VFQIS/VHLEIS/VLLS arneses entre VFCU/VLCU y los conectores de pared en los tanques de combustible. Estos arneses están identificados y remarcados como CDCCL en los procedimientos AMM correspondientes, para comprobar la correcta instalación, sin permitir alteraciones que puedan volar las limitaciones de la configuración critica de diseño del sistema ventral del indicador de cantidad de Combustible (VENTRAL FUEL QUANITY INDICATING SYSTEM) al igual que el Ventral del Sistema de Indicación de Exedencia de Alto Nivel (Ventral Low Level Switch) del arnés externo del tanque de combustible, debiendo cumplirse, cada vez que se realice cualquier tarea de mantenimiento, en cualquier área cercana a esta zona que pueda afectarse la instalación del arnés 3. Conector de bomba de combustible en pared de tanques de combustible Las bombas de combustible en los tanques principales y en los tanques auxiliares tienen conectores herméticos, los cuales están instalados y eléctricamente integrados a las paredes de los tanques: Este conector esta identificado y REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-3-10

remarcado como CDCCL en los procedimientos del AMM, deberán verificarse las superficies integradas en cualquiera de las bombas cuando estas sean cambiadas, asegurando la forma de cómo se encuentran integrados en cualquiera de los tanques de la aeronave. Esta lista, contiene las siguientes limitaciones: A.

B.

C.

Las características de los componentes identificados en esta lista deberán mantenerse en su configuración original, idéntica al tipo de diseño aprobado para la aeronave. Cualquier reparación o reparación mayor, a los componentes críticos de fuentes de ignición de cualquiera de los componentes identificados para el tipo de diseño aprobado de la aeronave, deberan mantenerse en esa condición, como lo muestra el manual de mantenimiento que es proporcionado por el titular del diseño aprobado o con las instrucciones especificas aprobadas por la Autoridad Certificadora de la reparación o reparación mayor. Cualquier alteración en las características de estos CDCCL´s en esta lista son clasificados como mayores y requieren una probación de la Autoridad Certificadora.

TAREAS RECOMENDADAS (Sección 12) Esta sección contiene las tareas recomendadas por Embraer, proveedores, MSG3 ISS y los grupos de trabajo que pretenden integrar a las tareas del MRB. Estas tareas están principalmente relacionadas a efectos económicos.

TAREAS DE COMPONENTES REEMPLAZO MANTENIMIENTO LINEA (Sección 13) Son tareas que se deben realizar a componentes específicos que debido a que pueden ser intercambiados entre aeronaves, resulta necesario realizar un seguimiento especial para cada uno. Estas tareas son controladas con referencia a los Ciclos y Horas de Vuelo de cada componente. El desarrollo de estas tareas se podrán realizar en todas las estaciones.

REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-3-11

TAREAS DE (Sección 14)

COMPONENTES

REEMPLAZO

MANTENIMIENTO

MAYOR

Son tareas que se deben realizar a componentes específicos que debido a que pueden ser intercambiados entre aeronaves, resulta necesario realizar un seguimiento especial para cada uno. Estas tareas son controladas con referencia a los Ciclos y Horas de Vuelo de cada componente. El reemplazo del componente se efectuara en las bases de mantenimiento de Aerolitoral que cuenten con el equipo necesario para realizar la remoción e instalación del componente así mismo bajo previa autorización de DGAC. TAREAS NO APLICABLES (Sección 15). Esta sección contiene la lista de Tareas establecidas en el MRBR que No son aplicables a las Aeronaves de Aerolitoral.

FORMATOS DE TAREAS INTERNAS (Sección 16) Contiene la lista y los Formatos a utilizar para el registro de los trabajos de mantenimiento programado emitidos por Aerolitoral. Las tareas en esta sección pueden ser las desarrolladas por el Departamento de Ingeniería además de las tareas del manual AMM del fabricante seleccionadas por el mismo departamento, que tienen como fin de mejorar el mantenimiento de las aeronaves. Las tareas de esta sección no son obligatorias, por lo tanto quedan a consideración de Aerolitoral su modificación y/o eliminación.

REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

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Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 1 Fecha Efectividad: 20-Sep-09 Pág. 1-4-1

1.4 DEFINICIÓN DE SERVICIOS Servicios Menores:

Servicio de 48 HR El servicio de 48 Horas se realiza cada 48 horas transcurridas por personal de línea. Este servicio incluye únicamente la verificación de la presión de las ruedas del Tren Principal y del Tren de Nariz. Al mismo tiempo se atienden los reportes abiertos de la bitácora de mantenimiento y se llevan a cabo las acciones correctivas necesarias. La periodicidad se suspenderá cada vez que el avión requiera mas de un día calendario fuera de servicio para realizar tareas de mantenimiento. En tal caso, el servicio de 48 horas debe ser efectuado antes de que el avión regrese a servicio, reasumiendo entonces su periodicidad. Este servicio no incluye tareas de ningún otro servicio, ni incluye en su totalidad a ningún otro servicio.

10 DY (LC1) “Line Check 1” El servicio LC1 se realiza cada 10 días calendario por personal de línea. El servicio LC1 examina el interior y el exterior del avión por condición y seguridad, así mismo se revisan operacionalmente los sistemas de detección de humo del baño y compartimento de carga, se revisa el equipo semifijo y al mismo tiempo se atienden los reportes abiertos de la bitácora de mantenimiento y se llevan a cabo las acciones correctivas necesarias. La periodicidad se suspenderá cada vez que el avión requiera más de seis días calendario fuera de servicio para realizar tareas de mantenimiento. En tal caso, la revisión LC1 debe ser efectuada antes de que el avión regrese a servicio, reasumiendo entonces su periodicidad. Este servicio contiene actividades del MRBR de 100 FH ó 14 días calendario, y algunas de 500 FH, 1 MO y 6 MO. Este servicio no incluye tareas de ningún otro servicio, ni incluye en su totalidad a ningún otro servicio.

40 DY (LC2) “Line Check 2” El servicio LC2 se realiza cada 40 días calendario por personal de línea. El servicio LC2 incluye pruebas operacionales y funcionales, así como la verificación de la cantidad de aceite del APU. Al mismo tiempo se atienden los reportes abiertos de la bitácora de mantenimiento y se llevan a cabo las acciones correctivas necesarias. Este servicio solo contiene actividades del MRBR de 400 FH. Este servicio no incluye tareas de ningún otro servicio, ni incluye en su totalidad a ningún otro servicio. REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 1 Fecha Efectividad: 20-Sep-09 Pág. 1-4-2

Servicios Intermedios:

Servicio de 4000 FH Este servicio se efectúa cada 4000 FH y contiene tareas de inspección visual detallada así como tareas operacionales. Este servicio no incluye tareas de ningún otro servicio, ni incluye en su totalidad a ningún otro servicio. Servicio de 8000 FH Este servicio se efectúa cada 8000 FH y contiene tareas funcionales y operacionales. Este servicio no incluye tareas de ningún otro servicio, ni incluye en su totalidad a ningún otro servicio. Servicio “A1” El servicio “A1” se efectúa cada 500 FH. Este servicio no incluye tareas de ningún otro servicio, ni incluye en su totalidad a ningún otro servicio. Servicio “A2” El servicio “A2” se efectúa cada 1000 FH. Este servicio no incluye tareas de ningún otro servicio, ni incluye en su totalidad a ningún otro servicio.

Servicio “A5” El servicio “A5” se efectúa cada 2500 FH. Este servicio no incluye tareas de ningún otro servicio, ni incluye en su totalidad a ningún otro servicio.

Servicios Mayores: Servicio “1C” El servicio “1C” se efectúa cada 5000 FH, 5000 FC ó 30 Meses (lo que ocurra primero). Este servicio contiene actividades del MRBR de 5000 FH, 5000 FC y 30 meses. Este servicio no incluye tareas de ningún otro servicio, ni incluye en su totalidad a ningún otro servicio. El Servicio “1C” se ha fraccionado en su formato con cuatro sub-clasificaciones: “1C” Sistemas, “1C” Estructural, “1C” CPCP y “1C” Zonal. REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

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Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 1 Fecha Efectividad: 20-Sep-09 Pág. 1-4-3

El cumplimiento de estos cuatro fraccionamientos del formato asegura el cumplimiento del Servicio “1C” en su totalidad. Servicio “2C” El servicio “2C” se efectúa cada 10,000 FH, 10,000 FC ó 60 Meses (lo que ocurra primero). Este servicio contiene actividades del MRBR de 10,000 FH, 10,000 FC y 60 meses. Este servicio no incluye tareas de ningún otro servicio, ni incluye en su totalidad a ningún otro servicio. El Servicio “2C” se ha fraccionado en su formato con cuatro sub-clasificaciones: “2C” Sistemas, “2C” Estructural, “2C” CPCP y “2C” Zonal. El cumplimiento de estos cuatro fraccionamientos del formato asegura el cumplimiento del Servicio “2C” en su totalidad. Servicio “4C” El servicio “4C” se efectúa cada 16,000 FH, 16000 FC ó 96 Meses (lo que ocurra primero). Este servicio contiene actividades del MRBR de 16,000 FH, 16,000 FC y 96 meses. Este servicio no incluye tareas de ningún otro servicio, ni incluye en su totalidad a ningún otro servicio. El Servicio “4C” se ha fraccionado en su formato con tres sub-clasificaciones: “4C” Estructural, “4C” CPCP y “4C” Zonal. El cumplimiento de estos tres fraccionamientos del formato asegura el cumplimiento del Servicio “4C” en su totalidad.

Servicios Estructurales Intermedios: Los Servicios Estructurales “E” comprenden tareas de “CPCP’s, Zonales y Estructurales”, mismas que se integran de la siguiente forma:

Servicios “E (2500 FC)” y “E (2500 FC) Empenaje” Estos servicios se efectúan cada 2500 ciclos de vuelo respectivamente. Estos servicios se han dividido en dos fases con mismo intervalo para facilidad de mantenimiento y las tareas contenidas son básicamente de Inspección Visual General y de Inspección Detallada. Estos servicios no incluyen tareas de ningún otro servicio, ni incluye en su totalidad a ningún otro servicio. REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 1 Fecha Efectividad: 20-Sep-09 Pág. 1-4-4

Servicios Estructurales Mayores: Servicios “E ( )” Los servicios codificados con “E” corresponden a los que contienen tareas estructurales aplicables a la aeronave en los intervalos indicados entre paréntesis. Ejemplo: E (30,000 FC) Servicio estructural a los 30,000 ciclos de vuelo. Servicios “E (x + y)” Los servicios codificados con E (x + y) corresponden a los que contienen tareas estructurales aplicables a la aeronave que cuentan con un Umbral para la primera aplicación indicada en “x” y posteriormente a intervalos repetitivos “y”, considerando su factor de repetitividad en FC, FH ó Meses. Ejemplo: E (20,000 FC + C1) Servicio estructural con un umbral de aplicación por primera vez a los 10,000 FC y una aplicación repetitiva a intervalos “C1” equivalente a 5000 FC. ó E (96 Months + C2) Servicio estructural con un umbral de aplicación por primera vez a los 96 Meses y una aplicación repetitiva a intervalos “C2” equivalente a 60 meses. Servicio Previo al Invierno (Prior to Winter) Comprende tareas que deben realizarse entre los meses de Octubre a Enero para tener en óptimas condiciones el avión en la época de invierno.

REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

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Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 1 Fecha Efectividad: 20-Sep-09 Pág. 1-5-1

1.5 CAMBIO DE LOS INTERVALOS DE INSPECCIÓN / MANTENIMIENTO.

Los tiempos límite que se muestran en el programa de mantenimiento pueden ser aumentados ó disminuidos de acuerdo a las condiciones que se muestran en el documento MRBR vigente de la aeronave Embraer EMB-145. De igual manera la aplicación de las tares podrá extenderse su periodo máximo de aplicación de acuerdo a las necesidades de operación de la flota de Aerolitoral, y en base a lo establecido por el manual SRMD vigente. Todas las tareas recomendadas así como las tareas internas de aerolitoral se consideran opcionales por lo que su limite de no es estrictamente fijo u obligatorio, son solo como referencia para su programación.

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Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-6-1

1.6 PROGRAMA DE LOS MOTORES Y APU La lógica MSG-3 se usó para desarrollar el programa de mantenimiento, el cual incluye los requerimientos de inspecciones periódicas especificados por Allison para el programa de mantenimiento del motor a condición. Para las inspecciones recomendadas e intervalos relacionados con este programa se usó la última revisión del Capítulo 5 del Manual de Mantenimiento AE 3007 A. En adición a los requerimientos de inspección programados, el programa del motor a condición, requiere que Aerolitoral realice un monitoreo de la operación del motor a través de información obtenida de: • • • • •

Instrumentos de motores en cabina de pilotos (EICAS) Mensajes en cabina de pilotos (EICAS) Mensajes de mantenimiento en cabina de pilotos (MFD) Datos de Mantenimiento del avión (CMC) Análisis del Programa de Monitoreo del motor

Proceso de Monitoreo de Motores: El Monitoreo de Motores consiste en que el personal Técnico descargue de la FADEC la información de los motores por medio de la CMC, posteriormente la información es archivada y consultada por el Ingeniero de Motores, quien es responsable de enviar la información a la compañía “Data Systems & Solutions (DS-S)” para su análisis y a su vez procesar la información en el programa “Compass Navigator”. Si existe una alerta la compañía (DS-S) y Allison envían al Ingeniero de Motores mediante correo electrónico, teléfono o fax las acciones correctivas a implementar. Este programa también incluye los requerimientos de inspección periódicos especificados por Sundstrand para el APU, para los cuales se usó la última revisión de las publicaciones de Sundstrand listadas en el apéndice 6 del MRBR.

REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

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Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-7-1

1.7 DEFINICION DE TERMINOS Lubricación (LUB) o Servicio (SVC). Cualquier acción de lubricar o dar servicio con el propósito de mantener las capacidades de diseño inherentes. Revisión Visual (VCK) o Revisión Operacional (OPC). Son tareas de observación para determinar que un componente esta cumpliendo completamente sus propósitos. No requiere tolerancias cuantitativas. Revisión Funcional (FNC). Es una revisión cualitativa o cuantitativa que determina que una o más funciones de un componente están dentro de los límites o estándares establecidos. Restauración (RST). Es el trabajo (dentro o fuera del avión) necesario para retornar un componente a un estándar específico. Descartar (DIS). La remoción de un componente del servicio a un límite de vida especifico. Inspeccion Visual General (GVI) Es un examen visual de un área interior o exterior, instalación o ensamble para detectar daños obvios, fallas o irregularidades. Este nivel de inspección se hace bajo condiciones de iluminación normalmente disponibles tales como luz de día, luces de hangar o linternas, y puede requerir abrir o remover paneles de acceso o puertas. Se pueden requerir plataformas de trabajo, escaleras o rampas para tener acceso al área a ser revisada. Inspección Visual Detallada (DVI) Es un examen visual intensivo de un área estructural específica, sistema, instalación o ensamble para detectar daños, fallas o irregularidades. La iluminación disponible normalmente es complementada por una fuente directa de iluminación de alta intensidad, con control de intensidad de luz ajustable por el inspector. Se pueden usar ayudas de inspección tales como espejos, lupas, etc. Se pueden requerir elaborados procedimientos de acceso y limpieza.

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Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

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Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-7-2

Inspección Especial Detallada (SDI) Es un examen intensivo de un componente específico, instalación o ensamble para detectar daños, fallas o irregularidades. El examen requiere uso extensivo de técnicas de inspección especializadas y/o equipo. Se pueden requerir procedimientos de desarmado o acceso, y limpieza profunda. Corrosión Nivel I Corrosión que ocurre entre inspecciones sucesivas, que es local y que puede ser retrabajada o removida dentro de los limites permitidos por el fabricante (SRM, SB, etc.), ó Corrosión que ocurre entre inspecciones sucesivas, que excede límites permitidos, pero que es local y puede ser atribuida a un evento no típico de uso del operador en otros aviones de la misma flota (P.E. Derramamiento de Mercurio), ó La experiencia del operador en las anteriores inspecciones ha demostrado solo corrosión ligera entre inspecciones sucesivas, pero la última inspección ahora excede los límites permitidos. Corrosión Nivel II La Corrosión Nivel II es un daño que ocurre entre inspecciones sucesivas que requiere un retrabajo, y entonces excede los limites permitidos, requiriendo una reparación / refuerzo, ó reemplazo parcial / total de un SSI, ó Un daño que ocurre entre inspecciones sucesivas que es extendida y requiere retrabajo aproximándose a los limites permitidos de retrabajo. Corrosión Nivel III La Corrosión Nivel III es un daño encontrado durante la primera, o subsecuentes inspecciones, que se determina que afecta la aeronavegabilidad, y por lo tanto requiere acción expedita. Componente de Mantenimiento Significante (Maintenance Significant Items-MSI) Los MSI´s son aquellos componentes identificados por Embraer cuya falla: I. Podría afectar la seguridad (en tierra o en vuelo), y/o II. Podría ser indetectable o no fácilmente detectable durante la operación, y/o III. Podría tener un significante impacto operacional, y/o IV. Podría tener un significante impacto económico.

REV. 01

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

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Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-7-3

Componente Estructural Significante (Structural Significant Item-SSI) Es cualquier elemento o ensamble estructural que contribuye significativamente a soportar cargas en vuelo, tierra, de presurización, o de control, y cuya falla podría afectar la integridad estructural necesaria para la seguridad de la aeronave. Límite de Tiempo (componente): Es un proceso primario de mantenimiento preventivo el cual requiere que la parte o componente sea reparado totalmente en un intervalo específico (Overhaul) de acuerdo con los manuales de los fabricantes o que esta sea removida de servicio. Límite de Vida (componente): Es un proceso de mantenimiento preventivo el cual requiere que la parte o componente sea removido de servicio de la aeronave y desechado a un tiempo específico.

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Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

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Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-8-1

1.8 ABREVIATURAS Y ACRONIMOS ABREVIATURAS AH CAT DET DIS DY FR FR FNC FUS IN LUB LWR MO OPC OVHT RST SDE SVC SYS VCK YR -

APU OPERATING HOURS CATEGORY DETAILED INSPECTION DISCARD DAY FRAME FRAME FUNCTIONAL CHECK FUSELAGE INSPECTION LUBRICATION LOWER MONTH OPERATIONAL CHECK OVERHEAT RESTORATION SPECIAL DETAILED INSPECTION SERVICE CHECK SYSTEM VISUAL CHECK YEAR

ACRONIMOS AC ACO AD ADC AFCS AHRS AMTOSS AOA APU ASSY ATA ATS BITE CAA CCMR CMC CMM REV. 01

ADVISORY CIRCULAR AIRCRAFT CERTIFICATION OFFICE ACCIDENTAL DAMAGE AIR DATA COMPUTER AUTOMATIC FLIGHT CONTROL SYSTEM ATTITUDE AND HEADING REFERENCE SYSTEM AIRCRAFT MAINTENANCE TASK ORIENTED SUPPORT SYSTEM ANGLE OF ATTACK AIRBORNE POWER UNIT ASSEMBLY AIR TRANSPORT ASSOCIATION AIR TURBINE STARTER BUILT-IN TEST EQUIPMENT CIVIL AVIATION AUTHORITY(UNITED KINGDOM) CANDIDATE CERTIFICATION MAINTENANCE REQUIREMENT CENTRAL MAINTENANCE COMPUTER COMPONENT MAINTENANCE MANUAL

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-8-2

CMR CPCP CTA CVR DAC DAU DG DGAC DPI DRC DRT DSM EASA ECS ED EGPWS EICAS ELT EMB EMDP FAA FADEC FAR FC FCOC FD FDA FDR FDR FDMU FFS FH FPMU FSA FWD GPU GPWS GVI HIRF HP HPT HYD IRS IRU ISC REV. 01

CERTIFICATION MAINTENANCE REQUIREMENT CORROSION PREVENTION AND CONTROL PROGRAM CENTRO TÉCNICO AEROESPACIAL COCKPIT VOICE RECORDER DEPARTAMENTO DE AVIAÇÃO CIVIL (BRASIL) DATA ACQUISITION UNIT DIRECTIONAL GYRO DIRECCION GENERAL DE AERONAUTICA CIVIL (MEXICO) DIFFERENTIAL PRESSURE INDICATOR DATA RECORDING/CALCULATING DISCARD/REPLACE TASK DESIGN STANDARDS MANUAL EUROPEAN AVIATION SAFETY AGENCY ENVIRONMENTAL CONTROL SYSTEM ENVIRONMENTAL DETERIORATION ENHANCED GROUND PROXIMITY WARNING SYSTEM ENGINE INDICATION AND CREW ALERTING SYSTEM EMERGENCY LOCATOR TRANSMITTER EMBRAER ENGINE MOTOR DRIVEN PUMP FEDERAL AVIATION ADMINISTRATION (USA) FULL AUTHORITY DIGITAL ENGINE CONTROL FEDERAL AVIATION REGULATION FLIGHT CYCLE FUEL COOLED OIL COOLER FATIGUE DAMAGE FATIGUE DAMAGE ANALYSIS FATIGUE DAMAGE RATING FLIGHT DATA RECORDER FLAP DRIVE MOTOR UNIT FLAP FLEXIBLE SHAFT FLIGHT HOUR FUEL PUMP AND METERING UNIT FLAP SCREW-JACK ACTUATOR FORWARD GROUND POWER UNIT GROUND PROXIMITY WARNING SYSTEM GENERAL VISUAL INSPECTION HIGH INTENSITY RADIATED FIELD HIGH PRESSURE HIGH PRESSURE TURBINE HYDRAULIC INERTIAL REFERENCE SYSTEM INERTIAL REFERENCE UNIT INDUSTRY STEERING COMMITTEE

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

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Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-8-3

JAA JAR L/HIRFLG LH LP LPT MEL MMEL MFD MFR MLG MLGB MPD MPG MRB MRBR MRBRP MSG MSI MTB MTBF MTBUR MWG NAA NDI NDT NLG NRU PCA PCU PMI PPH PWG R&M RBHA RH RMU RR RTCA RVSM SDI SMRD SPS SRM REV. 01

JOINT AVIATION AUTHORITIES JOINT AIRWORTHINESS REQUIREMENTS (EUROPE) LIGHTING /HIGH INTENSITY RADIATED FILED LANDING GEAR LEFT HAND LOW PRESSURE LOW PRESSURE TURBINE MINIMUM EQUIPMENT LIST MASTER MINIMUM EQUIPMENT LIST MULTI-FUNCTION DISPLAY MANUFACTURER MAIN LANDING GEAR MAIN LANDING GEAR BAY MAINTENANCE PLANNING DOCUMENT MAINTENANCE PLANNING GUIDE MAINTENANCE REVIEW BOARD MAINTENANCE REVIEW BOARD REPORT MAINTENANCE REVIEW BOARD REPORT PROPOSAL MAINTENANCE STEERING GROUP MAINTENANCE SIGNIFICANT ITEM MOTOR TRANSMISSION BRAKE MEAN TIME BETWEEN FAILURES MEAN TIME BETWEEN UNSCHEDULED REMOVALS MECHANICAL WORKING GROUP NATIONAL AVIATION ADMINISTRATION NON-DESTRUCTIVE INSPECTION NON-DESTRUCTIVE TESTING NOSE LANDING GEAR NEUTRAL RECOVERY UNIT POWER CONTROL ACTUACTOR POWER CONTROL UNIT PRINCIPAL MAINTENANCE INSPECTOR POLICY AND PROCEDURES HANDBOOK POWERPLANT WORKING GROUP RELIABILITY AND MAINTAINABILITY REQUISITO BRASILEIRO DE HOMOLOGAÇÃO AERONÁUTICA RIGHT HAND RADIO MANAGEMENT UNIT ROLLS-ROYCE RADIO TECHNICAL COMMISSION FOR AERONAUTICS REDUCED VERTICAL SEPARATION MINIMUM SPECIAL DETAILED INSPECTION SCHEDULED MAINTENANCE REQUIREMENTS DOCUMENT STALL PROTECTION SYSTEM STRUCTURAL REPAIR MANUAL

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB-145 Maintenance Program SECCION 1. DESCRIPCION DEL PROGRAMA

Código: M-PME-01 Número de Revisión: 2 Fecha Efectividad: 05-Abr-10 Pág. 1-8-4

SSA SSI SWG TAI TAT TBD TBO TBR TC TCAG TCS TR WG WOW ZWG -

REV. 01

SYSTEM SAFETY ASSESSMENT STRUCTURAL SIGNIFICANT ITEM STRUCTURAL WORKING GROUP THERMAL ANTI-ICE TOTAL AIR TEMPERATURE TO BE DETERMINED TIME BETWEEN OVERHAULS TIME BETWEEN REMOVALS TYPE CERTIFICATE TRANSPORT CANADA AVIATION GROUP (CANADA) TOUCH CONTROL STEERING TEMPORARY REVISION WORKING GROUP WEIGHT-ON-WHEEL ZONAL WORKING GROUP

Este documento contiene información confidencial propiedad de Aerolitoral S.A. de C.V. la cual no debe ser reproducida en ninguna forma sin el permiso de Aerolitoral; las violaciones a esto serán sancionadas por las leyes nacionales e internacionales. / This document contains Aerolitoral, S.A. de C.V. confidential information, which may not be reproduced in any form without permission from Aerolitoral; violations to this will be sanctioned by national and international laws.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 2. REQUERIMIENTOS DE INSPECCION RUTINARIOS

Fecha de Efectividad: 05-Abr-10 Page: 2 -1- 1 .

“ROUTINE INSPECTION REQUIREMENTS” Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

12-11-03-680-001-A00

ROUTINE

SVC

7

Drain Fuel Tanks to Check for the Presence of Water

-

12-13-01-610-001-A00

ROUTINE

SVC

7

Hydraulic System Reservoir Fluid Level Check

-

26-14-00-710-001-A00

ROUTINE

OPC

8

Operationally Check Lavatory Smoke Detection System

-

26-15-00-710-001-A00

ROUTINE

OPC

8

Operationally Check Baggage Smoke Detection System

Applicable only for aircraft equipped with baggage compartment class "D"

-

100 FH / 14 DY

ALL

27-12-01-212-002-A03

ROUTINE

GVI

8

Inspect (Visual Inspection) Aileron PCA Rod Ends/Fitting Lugs for Integrity and General Condition

Applicable for P/N: 394900-1007 ONLY

-

100 FH / 14 DY

EMB-145 (ALL)

28-11-00-212-001-A00

ROUTINE

GVI

7

Visually Check Underwing Surfaces, Tank Access Panels, Dump Valves and Drain Valves for Absence of Fuel Leakage

-

100 FH / 14 DY

ALL

28-12-03-212-001-A00

ROUTINE

GVI

7

Visually Check NACA Air Inlet for Absence of Obstruction

-

28-20-00-212-001-A00

ROUTINE

GVI

7

29-10-04-710-001-A00

ROUTINE

OPC

8

30-00-00-710-001-A00

ROUTINE

OPC

8

Operationally Check Anti-Icing System Messages

-

32-10-00-211-001-A00

ROUTINE

VCK

9

Visually Check Main Landing Gear, Including Doors and Spring Cartridges

-

32-10-02-211-001-A00

ROUTINE

VCK

9

Visually Check MLG Shock Absorber Extension

-

32-20-01-211-001-A00

ROUTINE

VCK

9

Visually Check Nose Landing Gear and Spring Cartridges for Condition and Shock Absorber Extension

-

32-33-15-720-001-A00

ROUTINE

FNC

8

Functionally Check Landing Gear Accumulator Nitrogen PreCharge.

32-44-02-610-001-A00

ROUTINE

SVC

7

Parking/Emerg Brake Nitrogen Accumulator Pressure Charge

-

32-49-01-212-001-A00

ROUTINE

GVI

6

Inspect (Visual Inspection) MLG Tires for Wear and General Condition

-

32-49-02-212-001-A00

ROUTINE

GVI

6

Inspect (Visual Inspection) MLG Wheel Assembly

-

32-49-03-212-001-A00

ROUTINE

GVI

6

32-49-04-212-001-A00

ROUTINE

GVI

6

32-49-05-212-001-A00

ROUTINE

GVI

6

Descripción / Description

Visually Check Fuel Line Shroud Drains for Absence of Fuel Leakage Operationally Check Electric Motor-Driven Pump (EMDP) in AUTO and ON modes

Inspect (Visual Inspection) Brake Assembly for General Condition Inspect (Visual Inspection) NLG Tires for Wear and General Condition Inspect (Visual Inspection) NLG Wheel Assembly

-

Applicable ONLY for aircraft equipped with Side Hinged Main Door Model.

-

-

Intervalo Interval 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY

100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY

Efectividad Effect. ALL ALL ALL

ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 2. REQUERIMIENTOS DE INSPECCION RUTINARIOS

Fecha de Efectividad: 05-Abr-10 Page: 2 -1- 2 .

“ROUTINE INSPECTION REQUIREMENTS” Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

34-13-00-212-001-A00

ROUTINE

GVI

7

Inspect (Visual Inspection) Pitot/Static Ports for Absence of Foreign Matter

-

35-10-00-211-001-A00

ROUTINE

VCK

7

Check Crew Oxygen Pressure

-

35-11-03-211-001-A00

ROUTINE

VCK

7

Visually Check Oxygen Cylinder Pressure Relief Disc

-

49-11-01-212-001-A00

ROUTINE

GVI

7

Inspect (Visual Inspection) APU and Starter Generator Air Intake and Exhaust Ducts for Foreign Material or Obstruction

-

71-12-01-212-002-A00

ROUTINE

GVI

7

Inspect (Visual Inspection) Engine and Generator Cooling Air Inlets/Outlets for Absence of Foreign Matter

-

72-00-00-970-001-A00

ROUTINE

DRC

9

Engine Trend Download/Analysis

Descripción / Description

OR 75 FC, whichever occurs first

-

Intervalo Interval 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY 100 FH / 14 DY / 75 FC

Efectividad Effect. ALL ALL ALL ALL ALL ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 1 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

12-12-01-600-801-A

SYSTEMS

SVC

7

20-00-00-140-001-A00

SYSTEMS

RST

20-00-00-140-002-A00

SYSTEMS

RST

20-00-00-140-003-A00

SYSTEMS

RST

20-00-00-140-004-A00

SYSTEMS

RST

20-00-00-140-005-A00

SYSTEMS

RST

20-00-00-140-006-A00

SYSTEMS

RST

20-00-00-140-007-A00

SYSTEMS

RST

20-00-00-140-008-A00

SYSTEMS

RST

20-00-00-140-009-A00

SYSTEMS

RST

20-00-00-140-010-A00

SYSTEMS

RST

20-00-00-140-011-A00

SYSTEMS

RST

20-00-00-212-001-A00

SYSTEMS

GVI

Descripción / Description Check the Engine Oil Level on the sight gauge (LH and RH side) Note: For oil level check prior to the first flight of the day, fill the engine oil tank until the oil reaches the one quart mark on the sight gauge. Prior to flights other than the first flig Clean Center Fuselage III Lower Side including wiring, lines and omega beams (Zones: 151, 152, 153, 154, 155, 156). NOTE: EWIS Clean Center Fuselage III Lower Side including wiring, lines and omega beams (Zones: 151, 152, 153, 154, 155, 156, 157). NOTE: EWIS Clean Center Fuselage IV Lower Side including wiring, lines and omega beams (Zones: 161, 162). NOTE: EWIS Clean Center Fuselage IV Upper Side surrounding ELT unit (Zones: 263, 264). NOTE: EWIS Clean Rear Fuselage I Lower Side, including wiring and lines (Zones: 171, 172). NOTE: EWIS Clean Rear Fuselage I Lateral Side, including electronic rear compartment wiring (Zones: 271, 272). NOTE: EWIS Clean Center Fuselage II Lower Side including wiring, lines and omega beams (Zones: 141, 142). NOTE: EWIS Clean Center Fuselage I Lower Side including wiring, lines and omega beams (Zones: 131, 132). NOTE: EWIS Clean NLG & FWD Electronic Compartments, FWD Pressure Bulkhead Upper Side (Zones: 113, 114, 213, 214, 215, 216). NOTE: EWIS Clean Cockpit Lateral Side and FWD Pressure Bulkhead Upper Side (Zones: 221, 222, 223, 224). NOTE: EWIS Clean Cockpit Lower Side and FWD Pressure Bulkhead Lower Side (Zones: 121, 122, 123, 124). NOTE: EWIS Inspect (General Visual) Center Fuselage III Lower Side - EWIS Components of APU and Engines Generators Power cables, Hydraulic Pumps Power cables and wiring bundles (Zones: 151, 152, 153, 154, 155, 156). NOTE: EWIS

20-00-00-212-002-A00

SYSTEMS

GVI

Inspect (General Visual) Center Fuselage III Lower Side - EWIS Components of APU and Engines Generators Power cables, Hydraulic Pumps Power cables and wiring bundles (Zones: 151, 152, 153, 154, 155, 156, 157). NOTE: EWIS

20-00-00-212-003-A00

SYSTEMS

GVI

Inspect (General Visual) Center Fuselage IV Lower Side - EWIS Components of APU and Engines Generators Power cables, Hydraulic Pumps Power cables and wiring bundles (Zones: 161, 162). NOTE: EWIS

20-00-00-212-004-A00

SYSTEMS

GVI

20-00-00-212-005-A00

SYSTEMS

GVI

20-00-00-212-006-A00

SYSTEMS

GVI

Inspect (General Visual) Rear Fuselage I Lower Side - EWIS Components of APU and Engines Generators Power cables and wiring bundles (Zones: 171, 172 / Task applicable to Baggage Compartment Class D). NOTE: EWIS Inspect (General Visual) Rear Fuselage I Lateral Side - EWIS Components of Engines Generators Power cables and wiring bundles (Zones: 271, 272 / Task applicable to Baggage Compartment Class D). NOTE: EWIS Inspect (General Visual) Rear Fuselage I Upper Side - EWIS Components of wiring bundles (Zones: 273, 274 / Task applicable to Baggage Compartment Class D). NOTE: EWIS

Ref. RR MM 12-10-79-600-801

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

48 FH

ALL

2C

2C

EMB-145EU; EMB-145EP; EMB-145ER; EMB-135ER EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-145XR EMB-135LR EMB-135KE EMB-135KL

2C

ALL

4C

ALL

C

ALL

2C

ALL

2C

ALL

2C

ALL

4C

ALL

2C

ALL

2C

ALL

2C

EMB-145EU; EMB-145EP EMB-145ER; EMB-135ER

2C

EMB-145LR; EMB-145LU EMB-145MR; EMB-145MP EMB-145MK; EMB-145XR EMB-135LR; EMB-135KE EMB-135KL

2C

ALL

C

ALL

2C

ALL

2C

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 2 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

20-00-00-212-007-A00

SYSTEMS

GVI

20-00-00-212-008-A00

SYSTEMS

GVI

20-00-00-212-009-A00

SYSTEMS

GVI

20-00-00-212-010-A00

SYSTEMS

GVI

20-00-00-212-012-A00

SYSTEMS

GVI

20-00-00-212-013-A00

SYSTEMS

GVI

20-00-00-212-014-A00

SYSTEMS

GVI

Cat. Cat.

Intervalo Interval

Efectividad Effect.

2C

ALL

2C

ALL

2C

EMB-145EU; EMB-145EP EMB-145ER; EMB-135ER

2C

EMB-145LR; EMB-145LU EMB-145MR; EMB-145MP EMB-145MK; EMB-135LR EMB-135KE ;EMB-135KL

4C

ALL

Inspect (General Visual) Engine Pylon - EWIS Components of Engines Generators Power cables and wiring bundles (Zones: 414, 424). NOTE: EWIS

C

ALL

Inspect (General Visual) Engines - EWIS Components of Engines Generators Power cables (Zones: 415, 425). NOTE: EWIS

C

Descripción / Description Inspect (General Visual) Rear Fuselage I, Pressure Bulkhead Pressurized area side - EWIS Components of APU Power Cables and wiring bundles (Zones: 275, 276). NOTE: EWIS Inspect (General Visual) Rear Fuselage II, Structural area aft of rear pressure bulkhead - EWIS Components of Power cables and wiring bundles (Zones: 311, 312). NOTE: EWIS Inspect (General Visual) Wing-to-fuselage attachment fairings - ER models - EWIS Components of wiring bundles (Zones: 191, 192, 193, 194, 195). NOTE: EWIS Inspect (General Visual) Wing-to-fuselage attachment fairings - LR models - EWIS Components of wiring bundles (Zones: 191, 193, 194, 195). NOTE: EWIS Inspect (General Visual) NLG Electronic Compartment - EWIS Components of wiring bundles (Zones: 113, 114). NOTE: EWIS

Umbral Thrsld.

ALL EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-145XR EMB-135LR EMB-135KE EMB-135KL EMB-145EU EMB-145EP EMB-145ER EMB-135ER EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-145XR EMB-135LR EMB-135KE EMB-135KL EMB-145EU EMB-145EP EMB-145ER EMB-135ER

20-00-00-220-001-A00

SYSTEMS

DET

Inspect (Detailed Inspection) - EWIS Components of Wing Tank Unit Harness (Zones: 155, 156, 157, 531, 631, 541, 641). NOTE: EWIS

2C

20-00-00-220-002-A00

SYSTEMS

DET

Inspect (Detailed Inspection) - EWIS Components of Wing Tank Unit Harness (Zones: 531, 631, 541, 641). NOTE: EWIS

2C

20-00-00-220-003-A00

SYSTEMS

DET

Inspect (Detailed Inspection) - Electric Fuel Pump Connector (Zones: 155, 156, 157). NOTE: EWIS

2C

20-00-00-220-004-A00

SYSTEMS

DET

Inspect (Detailed Inspection) - Electric Fuel Pump Connector (Zones: 531, 631). NOTE: EWIS

2C

20-00-00-220-007-A00

SYSTEMS

DET

Inspect (Detailed Inspection) Wing Middle Section - EWIS Components of Pilot Valve harness inside the conduit (Zones: 541, 641). NOTE: EWIS

2C

ALL

20-00-00-220-008-A00

SYSTEMS

DET

Inspect (Detailed Inspection) Wing Middle Section - EWIS Components of Vent Valve harness inside the conduit (Zones: 541, 641). NOTE: EWIS

2C

ALL

20-00-00-220-009-A00

SYSTEMS

DET

4C

ALL

20-00-00-220-010-A00

SYSTEMS

DET

2C

ALL

20-00-00-220-011-A00

SYSTEMS

DET

2C

ALL

20-00-00-220-012-A00

SYSTEMS

DET

2C

ALL

Inspect (Detailed Inspection) FWD Electronic Compartment/FWD Pressure Bulkhead Upper Side - EWIS Components of wiring bundles (Zones: 213, 214, 215, 216). NOTE: EWIS Inspect (Detailed Inspection) Cockpit Lower Side - EWIS Components of Power cables (Zones: 123, 124). NOTE: EWIS Inspect (Detailed Inspection) Cockpit Lateral Side - EWIS Components of Power cables (Zones: 223, 224). NOTE: EWIS Inspect (Detailed Inspection) Center Fuselage I Lower Side - EWIS Components of APU and Engines Generators Power cables, Hydraulic Pumps Power cables and wiring bundles (Zones: 131, 132). NOTE: EWIS

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 3 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

20-00-00-220-013-A00

SYSTEMS

DET

21-20-00-710-001-A00

SYSTEMS

OPC

7

Operationally Check Air Conditioned Distribution System

21-21-00-720-001-A00

SYSTEMS

FNC

9

Functionally Check Display Ventilation System

21-23-05-710-001-A00

SYSTEMS

OPC

21-25-01-710-001-A00

SYSTEMS

OPC

8

21-26-00-710-001-A00

SYSTEMS

OPC

21-26-08-960-001-A00

SYSTEMS

21-26-08-960-001-A01

SYSTEMS

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

2C

ALL

-

2C

ALL

-

C

ALL

-

5A

ALL

Operationally Check Ram Air Valve

-

C

ALL

9

Operationally Check Electronic Compartment Ventilation System

-

C

ALL

DIS

9

Discard Exhaust Hoses of the Electronic Bay Compartment.

-

5A

ALL

DIS

9

Discard Exhaust Hoses of the Electronic Bay Compartment.

-

180MOS

ALL

Operationally check baggage compartment ventilation system (including high and low speed of fan)

-

A

ALL

-

C

ALL

-

5A

ALL

Descripción / Description Inspect (Detailed Inspection) Center Fuselage II Lower Side - EWIS Components of APU and Engines Generators Power cables, Hydraulic Pumps Power cables and wiring bundles (Zones: 141, 142). NOTE: EWIS

Operationally Check Toilet Gasper Hose Filter (if installed).

21-27-00-710-001-A00

SYSTEMS

OPC

9

21-27-02-640-001-A00

SYSTEMS

LUB

8

Lubricate baggage compartment check valves

8

Operationally check baggage compartment check valve (manual check for free movement and corrected seating)

21-27-02-710-001-A00

SYSTEMS

OPC

21-31-00-710-001-A00

SYSTEMS

OPC

9

Operationally Check Pressurization Control System in Manual Mode

21-31-00-720-002-A00

SYATEMS

FNC

8

Funtionally check outflow valves pressure relief devices

21-31-00-720-005-A00

SYSTEMS

FNC

9

Functionally check line for leakage

21-31-03-140-001-A00

SYSTEMS

RST

6

Clean Electropneumatic Outflow Valve (No-smoking flights).

21-31-03-140-001-A01

SYSTEMS

RST

6

Clean Electropneumatic Outflow Valve

21-31-04-140-001-A00

SYSTEMS

RST

6

Clean Pneumatic Outflow Valve (No-smoking flights).

21-31-04-140-001-A01

SYSTEMS

RST

6

Clean Pneumatic Outflow Valve

21-31-08-960-001-A00

SYSTEMS

DIS

6

Replace Air Filter Element (No-smoking flights).

21-31-08-960-001-A01

SYSTEMS

DIS

6

Replace Air Filter Element

21-51-00-710-001-A00

SYSTEMS

OPC

8

21-51-00-720-001-A00

SYSTEMS

FNC

21-51-00-720-003-A00

SYSTEMS

FNC

21-51-01-130-001-A00

SYSTEMS

RST

21-51-02-170-001-A00

SYSTEMS

21-51-10-710-001-A00

SYSTEMS

21-60-00-710-001-A00

SYSTEMS

22-11-00-710-001-A00 23-51-00-710-001-A00

NOTE: Initial inspection since new, "C" check.

Pre-Mod. SB 145-21-0013 (Not applicable Aerolitoral fleet) Post-Mod. SB 145-21-0013 (All ERJ-145 Aerolitoral fleet) Baggage compartment with ventilation system only (All Aerolitoral ERJ-145 fleet) Baggage compartment with ventilation system only (All Aerolitoral ERJ-145 fleet) Baggage compartment with ventilation system only (All Aerolitoral ERJ-145 fleet)

-

2C

ALL

6000 FH

ALL

-

2C

ALL

-

5A

ALL

-

2A

ALL

-

1000 FH

ALL

-

400 FH

ALL

-

3200 FH

ALL

-

1800 FH

ALL

Operationally Check Cooling Pack System to Verify ECS OFF Signal

-

C

ALL

6

Functionally Check Cooling Pack System

-

2C

ALL

8

Functionally Check Pack Duct Overtemperature Protection

-

C

ALL

6

Clean Pack Valve Filter Using Ultrasonic Method

-

5A

ALL

RST

6

Clean Dual Heat Exchanger and Visually Check condition of core

-

C

ALL

OPC

8

Operationally Check Pack Leak Switch

-

2C

ALL

OPC

9

Operationally Check Temperature Control

-

2C

ALL

SYSTEMS

OPC

9

Operationally Check AFCS Go-Around Mode.

-

C

ALL

SYSTEMS

OPC

8

Operationally Check Audio System Emergency Mode

-

A

ALL

23-60-00-720-001-A00

SYSTEMS

FNC

9

Functionally Check Static Discharger

-

8000 FH

ALL

23-71-00-710-001-A00

SYSTEMS

OPC

9

Operationally Check Voice Recorder 4 Channels and Area Microphone

23-71-02-710-001-A00

SYSTEMS

OPC

9

Operationally Check CVR Underwater Locator Beacon

Post-SB 145-21-0002 No-smoking flights. (All Aerolitoral ERJ-145 fleet) For smoking flights. (Not applicable Aerolitoral fleet) No-smoking flights. (All Aerolitoral ERJ-145 fleet) For smoking flights. (Not applicable Aerolitoral fleet) No-smoking flights. (All Aerolitoral ERJ-145 fleet) For smoking flights. (Not applicable All ERJ145 Aerolitoral fleet)

Also Check TCS Mode.

Or according to Local Authorities.

-

C

ALL

-

24 MOS

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 4 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

23-71-02-960-001-A00

SYSTEMS

DIS

9

24-31-00-710-001-A00

SYSTEMS

OPC

9

24-31-00-710-002-A00

SYSTEMS

OPC

9

24-31-01-900-001-A00

SYSTEMS

RST

7

Restore Main Generator

24-31-01-900-001-A01

SYSTEMS

RST

7

Restore Main Generator

24-34-00-710-001-A00

SYSTEMS

OPC

9

Operationally Check APU Generation Over current Protection Circuit

-

C

ALL

24-34-00-710-002-A00

SYSTEMS

OPC

9

Operationally Check APU Generation Switching Circuit

-

C

ALL

-

1200 AH

ALL

ALL

24-34-01-900-001-A00

SYSTEMS

24-34-01-960-001-A00

SYSTEMS

24-35-01-720-001-A00

SYSTEMS

24-35-01-900-001-A00

SYSTEMS

24-36-01-610-001-A00 24-36-01-610-001-A02

RST

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

(*)

ALL

Operationally Check Main Generation Switching Circuit

-

C

ALL

Operationally Check Main Generation Overcurrent Protection Circuit

-

C

ALL

Applicable to P/N: 30086-010 ONLY

-

3200 FH

ALL

Applicable to P/N: 30086-011 ONLY

-

4000 FH

ALL

Descripción / Description Discard CVR Underwater Locator Beacon Battery

(*) NOTE:ULB battery change in accordance with manufacturer's dataplate expiration date.

Comply with task from SMRD 24-34-01-900002-A00 with int. 800 FH. The task from MRBR and SMRD are performed througt the same task from AMM 24-34-01-900-801-A.

7

Restore APU Starter/Generator

DIS

7

Discard APU Starter/Generator Brushes

-

800 AH

FNC

8

Functionally Check Back-up Battery

-

6 MO

ALL

RST

8

Restore Back-up Battery

-

12 MOS

ALL

SYSTEMS

SVC

6

SYSTEMS

SVC

6

24-36-01-720-001-A00

SYSTEMS

FNC

24-36-01-900-001-A00

SYSTEMS

RST

24-40-00-720-001-A00

SYSTEMS

24-54-00-212-001-A00

Service Main Battery

Interval according to manufacturer's recommendation. MARATHON N/P: 32248-001 ONLY

-

500 FH

ALL

Service Main Battery

MARATHON M3 N/P: 32845-001 ONLY

-

2000 FH

ALL

6

Functionally Check Main Battery

SAFT N/P: 442CH1 ONLY

-

1000 FH

ALL

8

Restore Main Battery

SAFT N/P: 442CH1 ONLY

-

12 MOS

ALL

FNC

7

Functionally Check GPU Overvoltage Protection

-

C

ALL

SYSTEMS

GVI

7

Inspect (General Visual) PC Power Components

-

C

ALL

24-60-00-710-001-A00

SYSTEMS

OPC

8

Operationally Check Electrical Emergency Transfer Circuit

-

C

ALL

24-60-00-710-002-A00

SYSTEMS

OPC

9

Operationally Check Electrical Emergency Abnormal Alarm

-

A

ALL

25-11-01-140-001-A00

SYSTEMS

RST

8

ALL

SYSTEMS

DVI

8

-

4000 FH

ALL

25-21-00-212-001-A00

SYSTEMS

GVI

7

-

C

ALL

25-21-00-220-002-A00

SYSTEMS

DVI

8

-

C

ALL

25-60-00-212-001-A00

SYSTEMS

GVI

8

-

6 MO

ALL

25-60-02-900-001-A00

SYSTEMS

RST

8

Clean Flight Crew Seats Locking System Inspect (Detailed Inspection) Cockpit Seats for Security ofAttachment to the Track, Including Restraint System Inspect (General Visual) Passenger Seats (Fabric Cover, Tray,Safety Belt Integrity and attachment to the track) Inspect (Detailed Inspection) Flight Attendant Seats harness, Inertial reel for condition and the seat bottom for freedom ofmovement and returning back to upright position Inspect (General Visual) First Aid Kit and Medical Kit for condition and validation P/N 106 A, 6240-37, S6-01-0005-311, S6-01-0005-314, 7000400, 01-00-48, 25-60-109-2, 25-60-109SL, 01-70-90, LAI 5532, 4531 and 73S601005107 Restore Flotation Vest PN 3505-101CW, 3505-101W, 3500-111W and 2000-105Y.

A

25-11-01-220-001-A00

-

24 MO

ALL

25-60-02-900-001-A01

SYSTEMS

RST

8

-

48 MO

ALL

Restore Flotation Vest PN MK3.

Applicable to aircraft equipped with PC Power System.

In accordance with expiration date or Local Regulatory Authority Requirements. Every 24 MO after 120 MO from date of manufacture; every 12 MO after 168 MO from date of manufacturer; in accordance with expiration date or Local Regulatory Authority Requirements.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 5 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Descripción / Description

25-60-02-900-001-A02

SYSTEMS

RST

8

Restore Flotation Vest PN MK20SV and MK22SV.

25-60-02-900-001-A03

SYSTEMS

RST

8

Restore Flotation Vest PN 63600-501 (Vacuum Packed).

25-60-02-900-001-A04

SYSTEMS

RST

8

Restore Flotation Vest PN 35-21-02.

25-60-04-710-001-A00

SYSTEMS

OPC

8

Operationally Check Megaphone P/N ACR/EM-1A

25-60-04-960-001-A00

SYSTEMS

DIS

6

25-60-05-212-001-A00

SYSTEMS

GVI

8

25-61-00-212-001-A00

SYSTEMS

GVI

8

25-61-00-710-001-A00

SYSTEMS

OPC

8

Operationally Check Emergency Locator Transmitter System- Proper Operation- Crash Switch Operation

25-61-04-960-001-A00

SYSTEMS

DIS

8

Replace ELT battery ARTEX P/N: 452-0130

25-61-04-960-001-A01

SYSTEMS

DIS

8

Replace ELT battery SOCATA P/N: ELT90A2560102000

25-61-04-960-001-A02

SYSTEMS

DIS

8

Replace ELT battery ARTEX P/N 452-0133

26-15-00-720-001-A00

SYSTEMS

FNC

8

26-15-01-212-001-A00

SYSTEMS

VCK

8

26-15-01-960-001-A00

SYSTEMS

DIS

8

26-21-00-720-001-A00

SYSTEMS

FNC

9

26-21-02-280-001-A00

SYSTEMS

SDI

9

26-21-02-720-001-A00

SYSTEMS

FNC

9

-

12 MO

ALL

-

2C

ALL

-

12 MOS

ALL

-

12 MOS

ALL

-

26 MOS

ALL

-

48 MOS

ALL

-

60 MO

ALL

-

A / 3 MOS

ALL

-

4A

ALL

-

180 MOS

ALL

-

2C

ALL

-

12 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

-

72 MOS

ALL

-

2C

ALL

-

2C

ALL

-

12 MOS

ALL

-

60 MOS

ALL

Functionally Check Engine Fire Extinguishing System Inspect Engine Fire Extinguishing Bottle for Weight and Check Bottle Pressure Perform Hydrostatic Check of the Engine Fire Extinguishing Bottle

Discard Engine Fire Extinguishing Bottle Cartridges

26-21-05-720-001-A00

SYSTEMS

FNC

9

Functionally Check Two-Way "Tee" Check Valves Functionally Check APU Fire Extinguishing System (Between switch and bottle connector) and Verify APU isolation by APU Fuel Shutoff Valve actuation. Inspect APU Fire Extinguishing Bottle for Weight and Check Bottle Pressure Perform Hydrostatic Check of APU Fire Extinguishing Bottle

SYSTEMS

FNC

9

Or according to Local Authorities' requirements.Follow manufacturer's recommendation. Or according to Local Authorities' requirements. Follow manufacturer's recommendation. (*) ELT Battery change in accordance with manufactuirer data plate expiration date or Local Regulatory Authority Requirements . (*) ELT Battery change in accordance with manufactuirer data plate expiration date or Local Regulatory Authority Requirements ELT battery change in accordance with manufacturer data plate expiration date or Local Regulatory Authority Requirements.

Functionally Check JAMCO Baggage Compartment Smoke Detection System (actuating each smoke sensor in the baggage compartment with a smoke tester) Visually Check WALTER KIDDE Baggage Compartment Smoke Detection System Maintenance LED Discard JAMCO Baggage Compartment Smoke Detector

9

26-22-01-720-001-A00

ALL

Discard of Megaphone Batteries P/N ACR/EM-1A

DIS

9

120 MO

Inspect (General Visual) Cockpit Escape Rope P/N 120-15112-001 Inspect (General Visual) Emergency Locator Transmitter for Condition, Expiration Date of Battery, Proper Installation, Battery Corrosion and Leakage

SYSTEMS

SDI

-

ALL

26-21-04-960-001-A00

SYSTEMS

ALL

ALL

Functionally Check Engine Fire Extinguishing Bottle Pressure Switch

26-22-01-280-001-A00

20 MO

6 MO

9

9

-

12 MO

FNC

FNC

Efectividad Effect.

-

SYSTEMS

SYSTEMS

Intervalo Interval

-

26-21-03-720-001-A00

26-22-00-720-001-A00

Every 12 MO after 240 MO from date of manufacture; in accordance with expiration date or Local Regulatory Authority Requirements. Every 60 MO for sewn packed; in accordance with expiration date or Local Regulatory Authority Requirements. In accordance with expiration date or Local Regulatory Authority Requirements.

Umbral Thrsld.

Or according to Local Authorities Requirements OR check every third bottle weight inspection (whichever occurs first). Or according to Local Authorities Requirements. As per the manufacturer's recommendation, Check at each bottle Hydrostatic Test (60MOS). NOTE: Or in accordance with manufacturer’s recommendation. Or according to Local Authorities Requirements or check every third bottle weight inspection, whichever occurs first Or according to Local Authorities Requirements.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 6 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

26-22-02-720-001-A00

SYSTEMS

FNC

9

26-22-03-960-001-A00

SYSTEMS

DIS

9

Discard APU Fire Extinguishing Bottle Cartridges

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

60 MOS

ALL

-

72 MOS

ALL

Class "C" Baggage compartment only.

-

C

ALL

Class "C" Baggage Compartment only Perform an Hydrostatic Test at each 60 MOS (Applicable All Aerolitoral ERJ-145 Fleet)

-

12 MOS

ALL

-

60 MOS

ALL

-

120 MOS

ALL

-

2C

ALL

-

1 MOS

ALL

-

12 MOS

ALL

Descripción / Description Functionally Check APU Fire Extinguishing Bottle Pressure Switch

As per the manufacturer's recommendation, Check at each bottle Hydrostatic Test (60MOS). NOTE: Or in accordance with manufacturer’s recommendation.

26-23-00-720-001-A00

SYSTEMS

FNC

8

Functionally Check Baggage Fire Extinguishing System (covering the pressure Switch, Cartridge, Baggage Fire Extinguishing Switch and Electrical Hardware).

26-23-01-280-001-A00

SYSTEMS

SDI

6

Inspect Baggage Compartment Fire Extinguishing Bottles (high rate and metering) for weight.

26-23-01-720-001-A00

SYSTEMS

FNC

6

Perform Hydrostastic Check of Baggage Fire Extinguishing Bottles (HIGH RATE & METERING)

26-23-02-960-001-A00

SYSTEMS

DIS

6

Discard Baggage Fire Extinguishing Bottles (high rate and metering) Cartridges

26-23-04-720-001-A00

SYSTEMS

FNC

6

Functionally Check two way check "TEE" Valve

26-24-00-211-001-A00

SYSTEMS

VCK

8

Visually Check Portable Fire Extinguishers

26-24-00-280-001-A00

SYSTEMS

SDI

9

Inspect Portable Fire Extinguishing Bottle for Weight (See placard attached to the bottle.)

26-24-01-720-001-A00

SYSTEMS

FNC

8

Perform Hydrostatic Check of portable Fire Extinguishing Bottles (WETTING Agent Only) P/N 892480

(WETTING Agent Only) Or in accordance with Local Regulatory Authority Requirements (Not applicable All Aerolitoral ERJ145 fleet)

-

60 MOS

ALL

26-24-01-720-001-A01

SYSTEMS

FNC

8

Perform Hydrostatic Check of portable Fire Extinguishing Bottles (HALON Agent Only) P/N 100-9750, 466090, 898052, A352 Series and C352

(HALON Agent Only) Or in accordance with Local Regulatory Authority Requirements (Applicable All Aerolitoral ERJ-145 Fleet)

-

144 MOS

ALL

26-25-01-280-001-A00

SYSTEMS

SDI

6

12 MO

ALL

27-11-00-220-001-A00

SYSTEMS

DVI

8

C

ALL

27-11-00-640-001-A00

SYSTEMS

LUB

6

Inspect Lavatory Fire Extinguisher Bottle for Weight Inspect (Detailed Inspection) Aileron Primary Mechanical Control from Control Wheel to Aileron PCAs, Checking Cables Pulleys, NRUs, Quadrants, Disconnect System and Mechanical Links Lubricate Control Wheel Chain

27-11-00-720-001-A00

SYSTEMS

FNC

6

Functionally Check Aileron Primary Mechanical Control Backlash

27-11-01-720-001-A00

SYSTEMS

FNC

6

Functionally Check Tension of Aileron Control Cables

27-12-00-720-001-A00

SYSTEMS

FNC

8

Functionally Check Aileron Hydraulic Actuation

27-12-00-720-002-A00

SYSTEMS

FNC

8

Functionally Check Aileron Hydraulic Damping

27-12-00-720-003-A03

SYSTEMS

FNC

8

Functionally Check External Leakage of Aileron Hydraulic Actuator

27-12-00-720-003-A04

SYSTEMS

FNC

8

27-12-00-720-003-A05

SYSTEMS

FNC

8

27-12-01-212-001-A00

SYSTEMS

GVI

7

Functionally Check External Leakage of Aileron Hydraulic Actuator Functionally check External Leakage of Aileron Hydraulic Actuator for aircraft Certificated Under EASA Regulations Inspect (Visual Inspection) Aileron PCA Hoses

Class "C" Baggage compartment only 180 months from date of manufacture (DOM) or 120 from date of installation, whichever ocurs first. (applicable All Aerolitoral ERJ-145 Fleet) Class "C" Baggage compartment only (Applicable All Aerolitoral ERJ-145 fleet) Or according to Local Authorities' Requirements. Interval follows manufacturer's recommendation. Or according to Local Authorities Requirements. Interval follows manufacturer's recommendation.

-

C

ALL

Threshold at 3C For new cables, check tension of the cable loop affected at first A and 2A before escalating to C

3C

C

ALL

-

C

ALL

-

2C

ALL

Pre S.B. 145-27-0062 Only For aircraft under CTA/FAA certifications: "3A" – Pre-Mod SB 145-27-0063. For aircraft under CTA/FAA certifications: "5A" – Post-Mod SB 145-27-0063.

-

400 FH

EMB-145(ALL)

-

3A

EMB-145(ALL)

-

5A

EMB-145(ALL)

-

2A

EMB-145(ALL)

-

C

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 7 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

27-12-01-212-002-A04

SYSTEMS

GVI

8

Inspect (Visual Inspection) Aileron PCA Rod Ends/Fitting Lugs for Integrity and General Condition.

25 FH / 3 Days for a/c equipped with PCA PN 394900-1003 or PN 394900-1005 ONLY (Not applicable Aerolitoral ERJ145 fleet)

-

25 FH / 3 DY

EMB-145(ALL)

27-12-01-212-002-A05

SYSTEMS

GVI

AD

Inspect (Visual Inspection) Aileron PCA Rod Ends/Fitting Lugs For Integrity and General Condition

"A" - Post-Mod SB145-27-0061/-62 & SB14557-0019; Pre-Mod SB145-27-0063 COMPLY BAD 1999-02-01-R6 c) & AD 99-05-04

-

A

EMB-145(ALL)

27-12-01-212-002-A06

SYSTEMS

GVI

AD

Inspect (Visual Inspection) Aileron PCA Rod Ends/Fitting Lugs for Integrity and General Condition.

(*) NOTE: "2A" - Post-Mod SB145-27-0061/62/-63 & SB145-57-0019 (Applicable to aircraft under CTA/FAA Regulations) COMPLY BAD 1999-02-01-R6 d) & AD 99-05-04

-

2A

EMB-145(ALL)

-

2A

EMB-145(ALL)

-

A

EMB-145(ALL)

-

5A

EMB-145(ALL)

-

2A

EMB-145(ALL)

-

C

ALL

-

2A

EMB-145(ALL)

-

2A

EMB-145(ALL)

-

5A

EMB-145(ALL)

-

5A

EMB-145(ALL) ALL

Descripción / Description

(*) NOTE: "2A" - Post-Mod SB145-27-0061/-62 & SB145-57-0019 (Applicable to aircraft under EASA Regulations) (Not applicable All Aerolitoral ERJ145 fleet) Applicable to aircraft Post-Mod SB 145-270062 and Pre-Mod SB145-27-0063 for aircraft under ANAC/FAA Regulations Applicable to aircraft Post-Mod SB 145-270062 and Post-Mod SB145-27-0063 for aircraft under ANACFAA Regulations

27-12-01-212-002-A07

SYSTEMS

GVI

8

Inspect (Visual Inspection) Aileron PCA Rod Ends/Fitting Lugs for Integrity and General Condition.

27-12-01-720-001-A03

SYSTEMS

FNC

8

Functionally Check Aileron Actuator Damping Components and Monitoring Devices

27-12-01-720-001-A04

SYSTEMS

FNC

8

Functionally Check Aileron Actuator Damping Components and Monitoring Devices

27-12-01-720-001-A05

SYSTEMS

FNC

8

Functionally Check Aileron Actuator Damping Components and Monitoring Devices

27-12-01-720-002-A01

SYSTEMS

FNC

9

Functionally Check Aileron Actuator Force Fight.

27-12-01-720-002-A02

SYSTEMS

FNC

9

Functionally Check Aileron Actuator Force Fight.

27-12-03-212-001-A00

SYSTEMS

VCK

9

Inspect (Visual Inspection) Aileron Damper Rod Ends/Fitting Lugs for Integrity and General Condition.

27-12-03-720-001-A00

SYSTEMS

FNC

9

Functionally Check Aileron Damper Damping Force

27-12-03-720-002-A00

SYSTEMS

FNC

9

Functionally Check External Leakage of Aileron Damper

27-13-00-710-001-A00

SYSTEMS

OPC

8

Operationally Check Aileron Solenoid Manifold Shutoff Function

-

C

27-14-00-720-001-A00

SYSTEMS

FNC

9

Functionally Check Roll Trim

-

C

ALL

27-15-00-710-001-A00

SYSTEMS

OPC

8

Operationally Check Aileron Disconnect System

-

C

ALL

27-15-02-640-001-A00

SYSTEMS

LUB

8

2C

ALL

SYSTEMS

DVI

9

Lubricate Aileron Disconnect System Inspect (Detailed Inspection) Rudder Primary Mechanical Control Checking Cables, pulleys and Quadrants

-

27-21-01-220-001-A00

-

C

ALL

-

C

ALL

-

C

ALL

-

C

ALL

27-21-01-720-001-A00

SYSTEMS

FNC

9

27-21-02-220-001-A00

SYSTEMS

DVI

8

27-22-00-720-001-A00

SYSTEMS

FNC

9

Functionally Check Tension of Rudder Control Cables

Applicable to aircraft Post-Mod SB 145-270062 for aircraft under EASA Regulations (Not applicable All Aerolitoral ERJ-145 fleet) Applicable to aircraft Post-Mod SB 145-270062. under ANAC/FAA Regulations (Applicable All Aerolitoral ERJ145 fleet) Applicable to aircraft Post-Mod SB 145-270062 under EASA Regulations. (Not applicable All Aerolitoral ERJ145 fleet) Applicable to aircraft Post-Mod SB 145-270063, under ANAC/FAA certifications. Applicable to aircraft Post-Mod SB 145-270063, under ANAC/FAA certifications. Applicable to aircraft Post-Mod SB 145-270063, under ANAC/FAA certifications.

The plate mechanism is bench lubricated.

(*) NOTE: For new aircraft, check tension cable llop affected at first A and 2A. Before escalating to C

Inspect (Detailed Inspection) Rudder Main Control Feedback Path, PCU Requires Removal of Concentric and Eccentric Linkage and Mounting Points, Rudder Actuator Attachments, Hinges, and Pins. Connecting Rods. Functionally Check Rudder Backlash

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 8 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

27-22-01-720-001-A00

SYSTEMS

FNC

9

27-22-02-212-001-A00

SYSTEMS

GVI

27-31-00-720-001-A00

SYSTEMS

FNC

27-31-01-220-001-A00

SYSTEMS

DVI

6

Inspect (Detailed Inspection) Elevator Control Cables

27-31-01-720-001-A00

SYSTEMS

FNC

6

Functionally Check Tension of Elevator Control Cables

27-31-04-710-001-A00

SYSTEMS

OPC

9

Operationally Check Spring/Servo Tab

27-31-05-220-002-A00

SYSTEMS

DVI

8

Inspect (Detailed Inspection) Spring Tab Attachment Link

27-35-00-640-001-A00

SYSTEMS

LUB

8

Lubricate Elevator Disconnect System

27-35-00-710-001-A00

SYSTEMS

OPC

8

27-36-00-710-001-A00

SYSTEMS

OPC

8

27-36-00-720-001-A00

SYSTEMS

FNC

9

27-40-00-710-002-A00

SYSTEMS

OPC

Umbral Thrsld.

Descripción / Description

Intervalo Interval

Efectividad Effect.

-

C

ALL

6

Functionally Check Rudder Power Control Unit/Actuators Differential Pressure Inspect (Visual Inspection) Rudder Actuators

-

C

ALL

6

Functionally Check Elevator Primary Mechanical Control Backlash

-

C

ALL

-

C

ALL

-

C

ALL

-

A

ALL

9

(*) NOTE: For new cables, check tension cable loop affected at first A and 2A.

-

C

ALL

-

2C

ALL

Operationally Check Elevator Disconnect System

-

C

ALL

Operationally Check Stall Protection System

-

400 FH

ALL

Functionally Check ICE/SPS Speeds Interface Circuit

-

400 FH

ALL

-

C

ALL

Operationally Check Backup/Main Cut-out Switch and Quick Disconnect Switch Operationally Check Lockout Logic of Horizontal Stabilizer Control Unit. NOTE: Post-Mod SB 145-27-0106 Functionally Check Horizontal Stabilizer Backlash Inspect (Detailed Inspection) Horizontal Stabilizer Actuator Integrity and Attachments Service Horizontal Stabilizer Actuator and check for leakage

The plate mechanism is bench lubricated.

27-40-00-710-003-A00

SYSTEMS

OPC

9

27-40-00-720-001-A00

SYSTEMS

FNC

8

27-40-02-220-001-A00

SYSTEMS

DVI

8

27-40-02-610-001-A00

SYSTEMS

SVC

6

27-40-03-640-001-A00

SYSTEMS

LUB

6

27-51-00-212-001-A00

SYSTEMS

GVI

7

27-51-00-220-001-A00

SYSTEMS

DVI

6

Inspect (Detailed Inspection) Flap Flexible Shafts

-

C

ALL

27-51-00-610-001-A00

SYSTEMS

SVC

6

Service Flap Screw-jack Actuators Gearbox PRE-MOD SB 145-27-0118

-

C

ALL

27-51-00-610-001-A01

SYSTEMS

SVC

6

Service Flap Screw-jack Actuators Gearbox POST-MOD SB 145-27-0118

-

2C

ALL

27-51-00-640-001-A00

SYSTEMS

LUB

6

Lubricate Flap Screw-Jack Actuators (FSAs)

-

2A

ALL

27-51-01-720-001-A00

SYSTEMS

FNC

8

Functionally Check Flap Transmission Brake Holding Capability

-

5A

ALL

27-51-15-220-001-A00

SYSTEMS

DVI

8

Inspect (Detailed Inspection) Flap Rollers for Structural Integrity

-

2C

ALL

27-51-17-720-001-A00

SYSTEMS

FNC

8

Functionally Check MTB (Flap Drive Motor Unit) Holding Capability

-

C

ALL

27-53-00-710-001-A00

SYSTEMS

OPC

9

A

ALL

SYSTEMS

OPC

8

-

A

ALL

27-63-01-710-001-A00

SYSTEMS

OPC

9

Operationally Check FLAP FAIL Message Operationally Check of Take-off Flap Aural Warning and No Take-off Configuration Visual Warning Operationally Check Spoiler System

-

27-53-00-710-002-A00

-

C

ALL

27-70-00-710-001-A00

SYSTEMS

OPC

7

Operationally Check Mechanical Gust Lock Mechanism

27-70-00-720-001-A00

SYSTEMS

FNC

9

Functionally check the Gap of Elevator Secondary Stop.

27-71-00-220-001-A00

SYSTEMS

DVI

9

27-71-00-710-003-A00

SYSTEMS

OPC

9

28-11-04-710-001-A00

SYSTEMS

OPC

9

28-12-01-710-001-A00

SYSTEMS

OPC

9

Post-Mod SB 145-27-0106

-

A

ALL

-

4000 FH

ALL

-

C

ALL

-

2000 FH

ALL

Lubricate Main Pitch Trim Switches

-

5A

ALL

Inspect (Visual Inspection) Flap Mechanical Line

-

C

ALL

Inspect (Detailed Inspection) Electromechanical Gust Lock Mechanism Operationally Check Electromechanical Gust Lock Air/Ground Protection Logic. Operationally Check (Manual Check for free movement and sealing condition) Flap Valves (Ribs 1 and 7) Operationally Check (Manual Check) Vent Float Valves (Rib 19)

Mechanical Gust Lock System ONLY Mechanical Gust Lock System ONLY Pre-Mod. S.B. 145-27-0079

-

C

ALL

-

4000 FH

ALL

Electromechanical Gust Lock System ONLY)

-

C

ALL

Electromechanical Gust Lock System ONLY

-

A

ALL

Check during Internal Tank Inspection.

-

2C

ALL

Check during Internal Tank Inspection.

-

2C

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 9 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

28-12-04-710-001-A00

SYSTEMS

OPC

9

28-12-05-211-001-A00

SYSTEMS

VCK

8

28-12-05-710-001-A00

SYSTEMS

OPC

8

28-21-03-720-001-A00

SYSTEMS

FNC

9

28-21-04-710-001-A00

SYSTEMS

OPC

9

Operationally Check Crossfeed Valve

-

C

ALL

28-21-10-710-001-A00

SYSTEMS

OPC

8

Operationally Check Fuel Feed Line Shroud

-

8000 FH

ALL

28-22-03-710-001-A00

SYSTEMS

OPC

8

8000 FH

ALL

SYSTEMS

OPC

9

-

C

ALL

28-41-01-720-001-A00

SYSTEMS

FNC

-

10000 FH

ALL

28-41-01-720-001-A01

SYSTEMS

FNC

-

10000 FH

ALL

28-43-00-720-001-A00

SYSTEMS

FNC

9

Operationally check APU Fuel Feed Line Shroud Operationally Check Electrical Fuel Quantity Indicating System (Fuel Low Level Logic) Functionally Check Fuel Conditioning (FCU) Functionally Check Fuel Conditioning (FCU) AD 2009-08-03 Functionally Check Fuel Temperature Indication System

-

28-41-00-710-001-A00

-

2C

ALL

28-44-00-720-001-A00

SYSTEMS

FNC

9

Functionally Check Low Level Warning System

-

2C

ALL

28-45-00-710-001-A00

SYSTEMS

OPC

9

Operationally Check Low Pressure Warning System

-

2A

ALL

28-50-01-220-001-A00

SYSTEMS

DET

8

Inspect (Detailed Inspection) Fuel Pump Electrical Harness

2C

ALL

Descripción / Description Operationally Check Flap Valve (Manual Check for Free Movement and Sealing Condition) Visually Check Flame Arrestor for Honey Comb Clogging, and Attaching Parts for Security Operationally Check Flame Arrestor in/out Flow Valves for Freedom Movement Functionally Check Relief Valve

Check during Internal Tank Inspection.

This task is comply with task 28-41-01-720001-A00 Check during Internal Tank Inspection.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

2C

ALL

-

C

ALL

-

C

ALL

-

2C

ALL

NOTE: EWIS/SFAR 88. This task complies with Fuel Tank Ignition Source Prevention (SFAR 88). NOTE: EWIS/SFAR 88. NOTE: This task complies with Fuel Tank Ignition Source Prevention (SFAR 88). NOTE: EWIS/SFAR 88.

2C

ALL

2C

ALL

2C

ALL

28-50-02-220-001-A00

SYSTEMS

DET

8

Inspect (Detailed Inspection) Wing Tank Unit

28-50-04-212-001-A00

SYSTEMS

GVI

8

Inspect (General Visual) Wing Stub Harnesses

28-50-05-212-001-A00

SYSTEMS

GVI

8

Inspect (General Visual) Trailing Edge Harnesses

28-50-06-212-001-A00

SYSTEMS

GVI

8

Inspect (General Visual) Leading Edge Harnesses

2C

ALL

29-10-00-710-001-A00

SYSTEMS

OPC

9

Operationally Check Electric Motor Driven Pumps Input Signals

-

C

ALL

29-10-00-790-001-A00

SYSTEMS

FNC

9

Functionally Check of Hydraulic Power System for Internal Leakage

-

2C

ALL

29-10-01-710-001-A00

SYSTEMS

OPC

8

29-10-04-900-001-A00

SYSTEMS

DIS

7

Operationally Check Shutoff Valve by means of the Hydraulic Panel Switch Replace EMDP Brushes

29-10-08-211-001-A00

SYSTEMS

VCK

9

Visually Check Differential Pressure Indicators for Red Pins Popped out

29-10-10-720-001-A00

SYSTEMS

FNC

8

29-10-13-720-001-A00

SYSTEMS

FNC

9

Functionally Check Return Filter By-Pass Valve NOTE: 2C if fluid contamination is checked at C interval. Functionally Check Priority Valve

29-30-03-720-001-A00

SYSTEMS

FNC

9

Functionally Check Hydraulic Filters Differential Pressure Indicators

29-30-05-710-001-A00

SYSTEMS

OPC

9

Operationally Check HYD SYS OVHT Message

30-11-05-710-001-A00

SYSTEMS

OPC

9

Operationally Check Wing Leak Thermostat

30-12-00-710-001-A00

SYSTEMS

OPC

8

Operationally Check Electrical Hardware of the Horizontal Stabilizer Thermal Anti-Icing System

30-12-05-710-001-A00

SYSTEMS

OPC

9

Operationally Check Horizontal Stabilizer Leak Thermostat

30-20-00-220-001-A00

SYSTEMS

DVI

9

30-20-01-720-001-A00

SYSTEMS

FNC

9

30-31-00-710-002-A00

SYSTEMS

OPC

9

Inspect (Detailed Inspection) Thermal Anti-Ice (TAI) Exhaust Duct for Condition and Security of Installation Functionally Check Thermal Anti-Ice (TAI) Interbulkhead Assembly for Leakage Operationally Check Pressurization Static Port Heating

2C if fluid contamination is checked at C interval. NOTE: 2C if fluid contamination is checked at C interval. Recommended task prior to the winter (October) in stead of “2C check” Recommended task prior to the winter (October) in stead of “C check” Recommended task prior to the winter (October) in stead of “2C check” Recommended task prior to the winter (October) in stead of “C check” Recommended task prior to the winter (October) in stead of “C check” Recommended task prior to the winter (October) in stead of “C check”

-

C

ALL

-

6000 FH

ALL

-

A

ALL

-

C

ALL

-

C

ALL

-

C

ALL

-

2C

ALL

2C

ALL

-

C

ALL

-

2C

ALL

-

C

ALL

-

C

ALL

-

C

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 10 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

30-31-00-710-001-A00

SYSTEMS

OPC

9

Operationally Check Pitot & Anemometric Static Port Heating

-

C

ALL

30-32-00-710-001-A00

SYSTEMS

OPC

9

Operationally Check AOA Sensor Heating

-

C

ALL

30-33-00-710-001-A00

SYSTEMS

OPC

9

Operationally Check TAT Sensor Heating

Descripción / Description

Intervalo Interval

Efectividad Effect.

-

C

ALL

-

C

ALL

ALL

30-42-00-710-001-A00

SYSTEMS

OPC

CATII

Operationally Check Windshield Heating

Recommended Task prior to the Winter (October) in stead of "C CHECK" and Maint. Program requirment for Cat. II Operation

31-21-00-710-001-A00

SYSTEMS

OPC

9

Operationally Check Digital Clock

Or according to Local Authorities' requirements. Check together with task 31-3100-710-001-A00.

-

12 MOS

31-31-00-710-001-A00

SYSTEMS

DRC

9

FDR Data-Personal computer Downloading

-

12 MOS

ALL

31-31-00-720-001-A00

SYSTEMS

FNC

6

Functionally Check Flight Data Recorder System

Or according to Local Authorities.

-

C

ALL

31-31-02-710-001-A00

SYSTEMS

OPC

9

Operationally Check FDR Underwater Locator Beacon

-

24 MOS

ALL

31-31-02-960-001-A00

SYSTEMS

DIS

9

Discard FDR Underwater Locator Beacon Battery

-

(*)

ALL

31-41-00-710-001-A00

SYSTEMS

OPC

9

Operationally Check DAU Channel Reversion Function

-

C

ALL

Restore Main Landing Gear (MLG) Leg Strut Assy (P/Ns 2309-2002series, 2309-3002-series, 2309-3100-series and-2309-4002-series)

-

144 MOS

ALL

32-10-01-900-001-A00

SYSTEMS

RST

8

32-10-01-900-002-A00

SYSTEMS

RST

8

32-10-02-610-001-A00

SYSTEMS

SVC

32-10-02-900-001-A00

SYSTEMS

32-10-03-900-001-A00

SYSTEMS

Or 20,000 FC, whichever occurs first.

-

144 MO

ALL

9

5A Or 15 MOS, whichever occurs first.

-

5A / 15 MOS

ALL

RST

8

Restore MLG Shock Absorber Assy (P/Ns 2309-2005-series)

20000 FC Or 144 MOS, whichever occurs first.

-

144 MOS

ALL

RST

8

20000 FC Or 144 MOS, whichever occurs first.

-

144 MOS

ALL

32-10-04-900-001-A00

SYSTEMS

RST

8

32-20-01-610-001-A00

SYSTEMS

SVC

9

32-20-01-720-001-A00

SYSTEMS

FNC

8

Functionally Check NLG Leg for Centering Cam Play

32-20-01-900-001-A00

SYSTEMS

RST

8

32-20-02-900-001-A00

SYSTEMS

RST

8

32-20-03-900-001-A00

SYSTEMS

RST

8

Restore NLG Auxiliary Drag Strut (P/Ns 1173B-series)

OPC

9

32-32-02-710-001-A00

SYSTEMS

OPC

8

32-34-00-640-001-A00

SYSTEMS

LUB

8

Lubricate Landing Gear (MLG & NLG) and Steering System

9

Operationally Check Landing Gear Emergency Extension (Override Switch)

32-34-00-720-001-A00

SYSTEMS

FNC

8

-

144 MOS

ALL

5A Or 15 MOS, whichever occurs first. 20000 FC Or 144 MOS, whichever occurs first. Perform at the opportunity of NLG leg strut Restoration.

-

5A / 15 MOS

ALL

-

144 MOS

ALL

-

144 MOS

ALL

Or 20000 FC whichever occurs first.

Operationally Check Landing Gear Extension and Retraction (Electrical) Indication and Downlock Relays by Channels A and B Operationally Check Solenoid and Downlock Release Button of the Landing Gear Control Lever

SYSTEMS

OPC

20000 FC Or 144 MOS, whichever occurs first.

Restore Nose Landing Gear (NLG) Strut (P/N 1170b0000-series; 1170C0000-series; 2233A0000-series; and 2666A0000), including 20000 FC Or 144 MOS, whichever occurs first. Torque Link, Steering cuff, sliding tube and web assy components; and their attaching parts Restore NLG Main Drag Strut (P/Ns 1172B0000-series and 1172C000020000 FC Or 144 MOS, whichever occurs first. series

32-32-00-710-001-A00

SYSTEMS

20000 FC Or 144 MOS, whichever occurs first.

Restore MLG Trailing Arm Assy (P/Ns 2309-2037-series, 2309-3037series and 2309-4037-series), including wheel axle Service MLG Shock Absorber

Restore MLG Main Side Strut(P/Ns 2309-2500-series and 2309-3500series) Restore MLG Secondary Side Strut Assy (P/Ns 2309-2600-series), including spring cartridges Service NLG Shock Absorber

32-34-00-710-001-A00

(*) NOTE:ULB battery change in accordance with manufacturer's dataplate expiration date.

Functionally Check Landing Gear Emergency Extension

"A" to aircraft Pre-Mod. SB 145-32-0036 and 145-32-0037. (Not applicable All Aerolitoral ERJ145 fleet)

-

20000 FC / 144 MOS 20000 FC / 144 MOS

ALL ALL

-

C

ALL

-

2C

ALL

-

400 FH

ALL

C

ALL

A

ALL

-

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 11 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

32-34-00-720-001-A01

SYSTEMS

FNC

8

Functionally Check Landing Gear Emergency Extension

-

C

ALL

32-34-03-720-001-A00

SYSTEMS

FNC

8

32-41-00-720-001-A00

SYSTEMS

FNC

6

Functionally Check Condition and Tension of Free-Fall Control Cables

-

2C

ALL

Functionally Check Main Brake System

-

C

32-41-01-710-001-A00

SYSTEMS

OPC

ALL

8

Operationally Check Brake Pedal Transducer

-

2C

ALL

32-41-07-720-001-A00

SYSTEMS

FNC

9

Functionally Check Brake Hydraulic Fuse

-

C

ALL

32-41-09-710-001-A00

SYSTEMS

32-44-00-720-001-A00

SYSTEMS

OPC

8

Operationally Check Return Line Check Valve of Main Brake System

-

C

ALL

FNC

8

Functionally Check Emergency Parking Brake System

-

2C

32-44-02-720-001-A00

ALL

SYSTEMS

FNC

8

Functionally Check Hydraulic Accumulator for Nitrogen Pre-Charge

-

2A

ALL

32-44-06-720-001-A00

SYSTEMS

FNC

8

-

2C

ALL

32-44-08-710-001-A00

SYSTEMS

OPC

8

-

C

ALL

-

C

ALL

-

ALL

-

48 FH 100 FH / 14 DY 100 FH / 14 DY 48 FH 100 FH / 14 DY A

ALL

32-44-10-640-001-A00

SYSTEMS

LUB

8

32-49-01-610-001-A00

SYSTEMS

SVC

6

32-49-02-220-001-A00

SYSTEMS

DVI

7

32-49-03-220-001-A00

SYSTEMS

DVI

6

32-49-04-610-001-A00

SYSTEMS

SVC

6

Descripción / Description

Functionally Check Thermal Relief Valve of the Emergency/ Parking Brake System Operationally Check Return Line Check Valve of Emergency/Parking Brake System Lubricate Mechanical Hardware (Handle) and Roller of Emergency Parking Brake Valve Check MLG Tire Inflation Pressure Inspect (Detailed Inspection) of Wheels Speed Transducer Clip in the Hub Cap Drive Clip (*) NOTE: At Each Tire Change only. Inspect (Detailed Inspection) of Brake Wear Indicator (*) NOTE: At Each Tire Change only. Check NLG Tire Inflation Pressure Operationally Check Brake Shuttle Valve. (*) NOTE: Or at each Brake Replacement only. Operationally Check Nose wheel Steering System Disengage

32-49-07-710-001-A00

SYSTEMS

OPC

8

32-50-00-710-001-A00

SYSTEMS

OPC

8

32-50-06-720-001-A00

SYSTEMS

FNC

8

32-62-00-710-001-A00

SYSTEMS

OPC

8

33-47-03-720-001-A00

SYSTEMS

FNC

8

33-47-03-720-001-A01

SYSTEMS

FNC

8

33-50-00-710-001-A00

SYSTEMS

OPC

8

Operationally Check Emergency Lighting System

33-50-04-720-001-A00

SYSTEMS

FNC

8

Functionally Check Emergency Lighting Battery Pack

33-50-12-280-001-A00

SYSTEMS

SDI

8

Inspect Photoluminescent Floor Proximity Strip Lights using Test Sample

33-50-12-720-001-A00

SYSTEMS

FNC

8

Functionally Check Photoluminescent Floor Proximity Strip Lights System

33-51-00-720-001-A00

SYSTEMS

FNC

8

Functionally Check Rechargeable Flashlight System (MODEL EF-2C)

33-51-00-720-001-A01

SYSTEMS

FNC

8

Functionally Check Non Rechargeable Flashlight System (MODEL EF-1)

"C" to aircraft Post-Mod. SB 145-32-0036 and 145-32-0037 (Applicable to all Aerolitoral ERJ fleet)

NOTE: At Each Tire Change only.

-

NOTE: At Each Tire Change only.

-

NOTE: Or at each Brake Replacement only.

Functionally Check 7-Degree Proximity Switch Operationally Check Landing Gear Warning System Functionally Check White Strobe Lighting System Pre-Mod. SB 145-33Applicable only to aircraft under ANAC/FAA 0008 NOTE: This task is applicable only to aircraft under ANAC/FAA certification (Applicable All Aerolitoral ERJ145 Certifications. fleet) Functionally Check White Strobe Lighting System Post-Mod. SB 145-330008 NOTE: This task is applicable only to aircraft under ANAC/FAA Certifications.

34-01-00-720-001-A00

SYSTEMS

FNC

CATII

Functionally Check Integrated Standby Instrument System - ISIS

34-11-00-720-001-A00

SYSTEMS

FNC

CATII

Functionally Check Standby Altimeter Indicator

NOTE: If installed.

Or according to Local Authorities requirements. Or according to Local Authorities requirements.

-

ALL ALL ALL ALL

-

C

ALL

-

A

ALL

-

800 FH

ALL

-

3A

ALL

-

400 FH

ALL

-

18 MOS

ALL

-

120 MO

ALL

-

C

ALL

2A

ALL

-

6 MOS

ALL

-

C

ALL

-

C

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 12 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

34-13-00-610-001-A00

SYSTEMS

SVC

6

Clean Pitot-Static System

34-13-00-680-001-A00

SYSTEMS

SVC

6

Drain Pitot Lines

34-13-00-680-001-A01

SYSTEMS

SVC

6

Drain Pitot Lines

34-13-00-790-001-A00

SYSTEMS

FNC

CATII

Functionally Check Pitot-Static System for Leakage

34-15-00-720-001-A00

SYSTEMS

FNC

CATII

Functionally Check ADC system

34-21-00-710-001-A00

SYSTEMS

OPC

9

Operationally Check AHRS DG Mode

34-21-03-140-001-A00

SYSTEMS

RST

6

34-22-00-710-001-A00

SYSTEMS

OPC

9

Clean AHRS Fan Filter Operationally Check Electronic Flight Instrument System Reversion Function

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

2C

ALL

-

C

ALL

-

A

ALL

-

C

ALL

-

C

ALL

-

C

ALL

-

2A

ALL

-

C

ALL

Or according to Local Authorities requirements.

-

24 MOS

ALL

Applicable to Dual IRS System Only

-

A

ALL

-

C

ALL

Descripción / Description

34-25-00-720-001-A00

SYSTEMS

FNC

6

Functionally Check Standby Compass for proper compensation

34-27-03-140-001-A00

SYSTEMS

RST

6

Clean Dual IRS Mounting Tray Fan Filter NOTE: Dual IRS System Only

Or according to Local Authorities Requirements. Pre-Mod SB 145-34-0021 Only (Not Applicable All Aerolitoral ERJ145 fleet) Post-Mod SB 145-34-0021 Only (Applicable All Aeritoral ERJ145 fleet) Or in accordance with local regulatory authority requirements Or in accordance with local regulatory authority requirements Applicable only to aircraft equipped with AHRS AH-800

Maintenance Program Requirement for Cat. II Operation Maintenance Program Requirement for Cat. II Operation Or according to Local Authorities

34-41-00-710-001-A00

SYSTEMS

OPC

CATII

Operationally Check GPWS/Windshear

34-41-00-710-003-A00

SYSTEMS

OPC

CATII

Operationally Check EGPWS/Windshear

34-52-00-720-001-A00

SYSTEMS

FNC

6

Functionally Check Transponder System

35-10-00-710-001-A00

SYSTEMS

OPC

8

Operationally Check Crew Oxygen Masks

-

C

ALL

35-10-00-710-001-A01

SYSTEMS

OPC

8

Operationally Check Crew Oxygen Mask Puritan and/or B/E Aerospace.

-

2350 FH

ALL

35-10-00-910-001-A00

SYSTEMS

FNC

REC

Leak Test Crew Oxygen System Lines

Together with Task 35-10-07-720-001-A00 and 35-10-07-720-002-A00

-

36 MOS

ALL

8

Functionally Check Crew Oxygen Cylinder Pressure Regulator NOTE: At the time of Cyl. Hydrostatic Test.

At the time of Cylinder Hydrostatic Test.

-

60 MOS

ALL

9

Functionally Check (Hydrostatic Test) Crew Oxygen Cylinder

Or according to Local Authorities requirements.

-

60 MOS

ALL

-

5A

ALL

-

4A

ALL

-

C

ALL

-

C

ALL

-

180 MOS

ALL

-

C

ALL

-

A

ALL

-

60 MOS

ALL

35-10-07-720-001-A00 35-10-07-720-002-A00

SYSTEMS SYSTEMS

FNC FNC

35-11-02-212-001-A00

SYSTEMS

VCK

8

Visually Check Pressure Transducer Indication on MFD Versus External Gauge Indication

35-20-00-710-001-A00

SYSTEMS

OPC

8

Operationally Check Passenger Oxygen System in MANUAL Mode

35-20-00-720-001-A00

SYSTEMS

FNC

9

Functionally Check Passenger Oxygen System in AUTO Mode

35-20-01-211-001-A00

SYSTEMS

VCK

8

Visually Check Chemical Oxygen Generator

35-20-01-960-001-A00

SYSTEMS

DIS

8

Replace/Discard Chemical Oxygen Generator

35-20-04-211-001-A00

SYSTEMS

VCK

8

Visually Check Passenger Oxygen Mask Visually Check Portable Oxygen Cylinder Gauge Pressure Indication (By convenience is comply each LC1) Functionally Check Portable Oxygen Cylinder Pressure Regulator NOTE: At the time of Cylinder Hydrostatic Test.

35-30-01-211-001-A00

SYSTEMS

VCK

9

35-30-01-720-001-A00

SYSTEMS

FNC

9

35-30-01-720-002-A00

SYSTEMS

FNC

9

Functionally Check (Hydrostatic Test) Portable Oxygen Cylinder

35-30-02-211-001-A00

SYSTEMS

VCK

9

35-30-03-960-001-A00

SYSTEMS

DIS

8

Visually Check Continuous Flow Mask Discard Protective Breathing Equipment PN MR10042N, 15-40F-11,1540F-10, 15-40F and E28180-10

Aircraft Equipped with Chemical Oxygen System Only. Aircraft Equipped with Chemical Oxygen System Only. Aircraft Equipped with Chemical Oxygen System Only. Aircraft Equipped with Chemical Oxygen System Only. Aircraft Equipped with Chemical Oxygen System Only. Or according to Local Authorities' requirements. At the time of Cylinder Hydrostatic Test. Or according to Local Authorities' requirements.

-

C

ALL

-

24 MOS

ALL

-

60 MOS

ALL

-

5A

ALL

-

120 MOS

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 13 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

36-10-01-130-001-A00

SYSTEMS

RST

6

36-11-01-220-001-A00

SYSTEMS

DVI

6

36-11-02-130-001-A00

SYSTEMS

RST

9

Clean Crossbleed Valve Filter by Ultrasonic Method Inspect (Detailed Inspection) Engine Low Pressure Bleed Air Check Valve. P/N 816603-3 Clean High-Stage Valve Filter by Ultrasonic Method

-

C

ALL

-

C

ALL

36-11-03-130-001-A00

SYSTEMS

RST

6

Clean Fan Air Valve Filter by Ultrasonic Method

-

C

ALL

-

C

36-11-04-110-001-A00

SYSTEMS

RST

6

Clean Pre-Cooler by Chemical Method

ALL

-

6000 FH

ALL

36-11-05-130-001-A00

SYSTEMS

RST

6

Clean Engine Bleed Valve Filter by Ultrasonic Method

36-20-00-710-001-A00

SYSTEMS

OPC

8

Operationally Check Bleed Valve Indicating Function

-

C

ALL

-

2C

36-20-00-720-001-A00

SYSTEMS

FNC

8

Functionally Check the Overtemperature Warning Circuit

ALL

-

2C

36-20-00-720-002-A00

SYSTEMS

FNC

9

Functionally Check Differential Pressure Protection Function

ALL

-

2C

ALL

36-20-02-710-001-A00

SYSTEMS

OPC

8

36-20-02-710-002-A00

SYSTEMS

OPC

8

Operationally Check Thermal Switch

-

2C

ALL

Operationally Check Massive Leakage Switch

-

C

ALL

38-32-04-960-001-A00

SYSTEMS

DIS

7

Replace Waste Drain Valve O'Ring

-

18 MOS

ALL

38-32-10-960-001-A00

SYSTEMS

DIS

7

Replace Waste Drain Valve Cap Seal

-

60 MOS

ALL

45-45-00-970-002-A00

SYSTEMS

DRC

7

CMC DATA - Personal Computer Downloading

-

A

ALL

49-17-00-160-001-A00

SYSTEMS

RST

9

Clean APU Drains Post-Mod SB 145-49-0029

-

C

ALL

49-19-00-160-001-A00

SYSTEMS

RST

Clean APU Drains (APU C14)

-

C

All

-

400 AH

ALL

-

800 AH

ALL

-

1200 AH

ALL

-

1200 AH

ALL

-

2C

ALL

-

400 AH

ALL

-

2000 AH

ALL

Descripción / Description

49-31-00-710-001-A01

SYSTEMS

OPC

9

Perform a Check of the FADEC BITE display for fault messages

49-31-04-960-001-A00

SYSTEMS

DIS

9

Replace/Discard Inlet Fuel Filter.

49-31-04-960-001-A01

SYSTEMS

DIS

9

Replace/Discard APS 500R Inlet Fuel Filter

49-41-03-220-001-A00

SYSTEMS

DVI

6

Inspect (Detailed Inspection) Igniter Plug Ref a 49-44-03-200-801-A

P/N 816603-3 ONLY

PRE SB 145-36-0028

PRE SB SB145-36-0018

Applicable for APU MODEL T-62T-40C14 (APS500R). Discard Inlet Fuel Filter APU Model T-62T40C11 (APS 500)only Applicable for APU MODEL T-62T-40C14 (APS500R). According to Manufacturer's recommendation.

Operationally Check Emergency Shutdown by Using APU Fuel Shutoff Switch and Fire Test Switch Check Oil Level and Service Oil System as required Ref a 49-96-00-200According to manufacturer's recommendation. 801-A

49-62-00-710-001-A00

SYSTEMS

OPC

9

49-91-00-610-001-A00

SYSTEMS

SVC

6

49-91-00-680-001-A00

SYSTEMS

SVC

9

Drain and Replace Oil Supply Ref a 49-96-00-600-801-A

According to manufacturer's recommendation.

49-91-01-960-001-A00

SYSTEMS

DIS

9

Replace/Discard Oil Filter Element Ref a 49-96-01-960-801-A

According to manufacturer's recommendation.

-

2000 AH

ALL

52-00-00-211-001-A00

SYSTEMS

VCK

7

Visually Check Locking Red Marks

Repaint if necessary.

-

C

ALL

5A

ALL

SYSTEMS

LUB

6

Lubricate Standard Main Door Actuating and Locking Mechanism

Only aircraft equipped with standard main door model.

-

52-00-04-212-001-A00 52-11-00-640-001-A00

GVI

52-11-00-640-002-A00

Inspect (General visual) Rubber Trim Seal

LUB

52-11-00-720-005-A00

SYSTEMS

FNC

8

52-12-00-710-001-A00

SYSTEMS

OPC

9

52-12-00-720-001-A00

SYSTEMS

FNC

7

52-14-00-220-001-A00

SYSTEMS

DVI

9

52-18-00-640-001-A00

SYSTEMS

LUB

6

52-18-00-640-002-A00

LUB

52-18-00-720-001-A00

FNC

Lubricate Standard Main Door Actuating and Locking Mchanism Functionally Check Standard Main Door Actuating, Latching and Locking Only aircraft equipped with standard main door Mechanism model. Only aircraft equipped with standard main door Operationally Check Alternate Opening System model. Only aircraft equipped with standard main door Functionally Check Main Door Hydraulic Accumulator Nitrogen Charge model. Inspect (Detailed Inspection) Main Door Draining System for Obstruction or Damage Only aircraft equipped with side hinged main Lubricate Side-Hinged Main Door Actuating and Locking Mechanism door model. Lubricate Side-Hinge Main Door Actuating and locking Mechanism Funtionally check Main-Door Internal Actuating Handle

C

ALL

5A

ALL

-

C

ALL

-

C

ALL

-

5A

ALL

-

C

ALL

-

C

ALL

5A

ALL

5A

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 14 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

52-18-06-720-001-A00

SYSTEMS

FNC

8

52-21-00-640-001-A00

SYSTEMS

LUB

52-21-00-710-001-A00

SYSTEMS

OPC

52-22-00-710-001-A00

SYSTEMS

52-22-01-640-001-A00 52-31-00-640-001-A00

52-18-04-960-001-A00

Cat. Cat.

DIS

Umbral Thrsld.

Descripción / Description

Only aircraft equipped with side hinged main door model.

8

Discard Side-Hinged Main Door Rubber Trim Seal Functionally Check Side-Hinged Main door Actuating, Latching and Locking Mechanism Lubricate Passenger Cabin Escape Hatch Support Pins

8

Operationally Check Passenger Cabin Escape Hatch Mechanism

Recommended task prior to the winter (October) in stead of “C check”

OPC

9

SYSTEMS

LUB

SYSTEMS

LUB

52-32-00-220-001-A00

SYSTEMS

DVI

7

52-42-01-220-001-A00

SYSTEMS

DVI

9

52-43-00-640-001-A00

SYSTEMS

LUB

6

52-43-06-720-001-A00

SYSTEMS

FNC

8

52-44-01-220-001-A00

SYSTEMS

DVI

9

52-51-00-720-001-A00

SYSTEMS

FNC

8

Intervalo Interval

Efectividad Effect.

C

ALL

-

C

ALL

-

C

ALL

-

C

ALL

Operationally Check Cockpit Emergency Exit

-

C

ALL

9

Lubricate Cockpit Emergency Exit Locking Mechanism

-

C

ALL

6

Lubricate Baggage Door Gear Box Inspect Baggage Door Lifting and Lowering Mechanism for General Condition and Torsion Bar for Torsion Inspect (Detailed Inspection) Cockpit Underfloor Access Hatch Mechanism Lubricate Service Door Actuating and Locking Mechanism Functionally Check Service Door Actuating, Latching and Locking Mechanism Inspect (Detailed Inspection) Rear Electronic Compartment Door Mechanism Functionally Check Reinforced Cockpit Door Operationally Check Forward Electronic Compartment Door Warning Message Operationally Check Rigging Door Warning Message

-

C

ALL

-

C

ALL

-

C

ALL

-

C

ALL

-

C

ALL

-

C

ALL

-

4000 FH

ALL

-

C

ALL

-

C

ALL

52-71-00-710-001-A00

SYSTEMS

OPC

8

52-72-00-710-001-A00

SYSTEMS

OPC

9

52-73-00-710-001-A00

SYSTEMS

OPC

9

Operationally Check Main Door Warning Message

-

C

ALL

52-73-01-720-001-A00

SYSTEMS

FNC

9

-

C

ALL

5A

ALL

5A

ALL

-

C

ALL ALL

OPC

9

Functionally Check Main Door Warning Microswitches Funtionally check Main Door Warning Microswitches (Standar Main Door Model) Funtionally check Main Door Warning Microswitches (Side Hinged Main Door Model) Operationally Check Service Door Warning Message

SYSTEMS

FNC

9

Functionally Check Service Door Warning Microswitches

-

C

SYSTEMS

OPC

8

Operationally Check Emergency Exit Warning Message

-

C

ALL

52-76-00-710-001-A00

SYSTEMS

OPC

8

-

C

ALL

52-77-00-710-001-A00

SYSTEMS

OPC

8

-

C

ALL

53-00-01-220-001-A00

SYSTEMS

DVI

9

Operationally Check Baggage Door Warning Message Operationally Check Rear Electronic Compartment Door Warning Message Inspect (Detailed Inspection) Fuselage Drain Valves for Obstruction or Damage Inspect (General Visual) Frame Rubber Seal

-

C

ALL

5A

ALL

53-21-02-140-001-A00

SYSTEMS

RST

7

Clean Main Door-Frame Rollers

-

C

ALL

53-21-02-640-001-A00

SYSTEMS

LUB

7

Lubricate Main Door Frame Rollers

-

A

ALL

53-21-12-140-001-A00

SYSTEMS

RST

7

Clean Service Door-Frame Rollers

-

C

ALL

53-21-12-640-001-A00

SYSTEMS

LUB

7

Lubricate Service Door Frame Rollers

-

A

ALL

71-10-00-211-001-A00

SYSTEMS

VCK

9

-

C

ALL

71-10-00-220-001-A00

SYSTEMS

DVI

9

-

C

ALL

71-20-00-220-001-A00

SYSTEMS

DVI

8

Visually Check Cowling Seals Inspect (Detailed Inspection) Cowling Inboard/Outboard Attachment and Surrounding structure Inspect (Detailed Inspection) Engine Elastomeric Mounts

-

C

ALL

71-60-01-211-001-A00

SYSTEMS

VCK

9

Visually Check Air Intake Attachment

-

C

ALL

71-60-01-211-002-A00

SYSTEMS

VCK

9

Visually Check Air Intake Rear Bulkhead and Fire Shield

-

C

ALL

72-21-01-220-001-A00

SYSTEMS

DVI

9

Inspect (Detailed Inspection) Fan Blades

-

4000 FH

ALL

52-73-01-720-002-A00

FNC

52-73-01-720-003-A00

FNC

52-74-00-710-001-A00

SYSTEMS

52-74-01-720-001-A00 52-75-00-710-001-A00

53-21-01-212-001-A00

GVI

Ref. Allison MM Section 5 Task 72-21-15-200801

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 15 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

72-21-20-220-001-A00

SYSTEMS

OPC

8

Inspect (detailed inspection) Fan Spinner Pre-Mod Rolls Royce SB 3007A-72-167 Only

72-63-01-710-001-A00

SYSTEMS

OPC

AD

Operationally Check Starter Drain Adapter

73-11-10-130-001-A00

SYSTEMS

RST

6

73-11-10-130-001-A01

SYSTEMS

RST

6

73-21-00-211-001-A00

SYSTEMS

VCK

9

Visually Check Fuel Pump and Metering Unit for Fuel Leakage

73-21-06-720-001-A00

SYSTEMS

FNC

9

73-22-01-720-003-A00

SYSTEMS

FNC

9

Functionally Check Fuel Filter Impending Bypass Indicating System Inspect Multi-Function Display for ENG( ) LT FAULT and ENG ( ) SCHED MAINT REPAIR Maintenance Messages

73-30-04-211-001-A00

SYSTEMS

74-21-01-220-001-A00 76-12-00-710-001-A00

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

A

ALL

Ref. Allison MM Section 5 Task 72-63-10-700801 Applicable Post SB AE3007A-72-330 and Pre-Mod SB AE3007A-72-330 (All Aerolitoral ERJ-145 fleet) COMPLY AD 99-02-51

-

800 FH

ALL

Clean Fuel Nozzles except P/N 23075904, P/N 23077006 and P/N 23087207

EXCEPT P/N: 23075904, P/N 23077006 and P/N 23087207 ONLY RR Task 73-11-10-000801 RR Task 73-11-10-400-801

-

2000 FH

ALL

Clean Fuel Nozzles

APPLICABLE TO P/N: P/N 23075904, P/N 23077006 and P/N 23087207 ONLY RR Task 73-11-10-000-801 RR Task 73-11-10-400-801

-

10000 FH

ALL

-

2A

ALL

-

3000 FH

ALL

-

500 FH

ALL

-

C

ALL

-

4000 FH

ALL

-

2C

ALL

Descripción / Description

VCK

9

Visually Check the FADEC Anti-Vibration Mounts

SYSTEMS

DVI

6

Inspect (Detailed Inspection) Ignitors

SYSTEMS

OPC

8

Operationally Check WOW input signal to Fadec

76-13-03-710-001-A00

SYSTEMS

OPC

8

Operationally Check Idle Lockout

76-20-00-710-001-A00

SYSTEMS

OPC

8

78-10-01-212-002-A00

SYSTEMS

GVI

8

Operationally Check Emergency Shutdown System Inspect (Visual Inspection) Plain Exhaust Assy for Damage, Failure or Irregularities

78-31-00-220-001-A00

SYSTEMS

DVI

9

Inspect (Detailed Inspection) Thrust Reverser Structure

78-32-00-211-001-A00

SYSTEMS

VCK

8

Visually Check Thrust Reverser 1RY and 3RY Locks

78-32-00-710-001-A00

SYSTEMS

OPC

8

Operationally Check Thrust Reverser 2RY and 3RY Locks

78-33-00-720-001-A00

SYSTEMS

FNC

9

Functionally Check Thrust Reverser Control Lever Microswitches

78-34-01-720-001-A00

SYSTEMS

FNC

AD

Functionally Check Stow/Transit Thrust Reverser Microswitches for insulation

79-25-02-211-001-A00

SYSTEMS

VCK

9

79-27-00-211-001-A00

SYSTEMS

VCK

9

79-34-00-212-001-A00

SYSTEMS

GVI

79-34-01-720-001-A00

SYSTEMS

79-37-00-720-001-A00

SYSTEMS

By convenience is comply each 2A

Comply RR Allison MM Section 5 Task 73-2510-000-801 Task 73-25-10-400-801 Ref. Allison MM Section 5 Task 74-21-10-200801 (All Aerolitoral ERJ-145 fleet) Only aircrafts with thrust reversers

-

A

ALL

-

5A

ALL

-

8000 FH

ALL

-

2C

ALL

-

A

ALL

-

2A

ALL

-

2C

ALL

-

1200 FH

ALL

Visually Check Fuel Cooled Assembly (FCOC)

-

2C

ALL

Visually Check Oil Plumbing

-

2C

AD

Inspect Multi-Function Display for ENG1(2) OIL DEBRIS Maintenance Message (Except for aircraft equipped with AE3007A1E Engine)

-

50 FH

ALL EMB-145EU EMB-145EP EMB-145ER EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-135ER EMB-135LR EMB-135KE EMB-135KL

FNC

9

Functionally Check Indicating Magnetic Plug Assembly

-

2C

ALL

FNC

9

Functionally Check Oil Filter Impending Bypass Indicating System

-

2C

ALL

Applicable to aircraft WITHOUT thrust reversers installed. Applicable to aircraft WITH thrust reversers installed. Applicable to aircraft WITH thrust reversers installed. Applicable to aircraft WITH thrust reversers installed. Applicable to aircraft WITH thrust reversers installed. Applicable to aircraft WITH thrust reversers installed. And applicable only for P/N’s 83-990137, 83-990-152 and 83-990-166. COMPLY AD 2001-17-03 paragraph b)

Ref. Allison MM Section 5 Task 79-37-10-700801 (All Aerolitoral ERJ-145 fleet) Ref. Allison MM Section 5 Task 79-37-15-700801 (All Aerolitoral ERJ-145 fleet)

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN3.REQUERIMIENTOSDEINSPECCIONDESISTEMASYPLANTAMOTRIZ

Fecha de Efectividad: 05-Abr-10 Page: 3 -1- 16 .

"SYSTEMS&POWERPLANTINSPECTIONREQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

80-10-01-720-001-A00

SYSTEMS

FNC

6

Functionally check Air Turbine Starter including oil servicing

A

ALL

Clean Start Control Valve Filter

To functionally check the air turbine Starter including oil servicing Applicable to Pre SB 145-80-0003 Only.

80-10-02-160-001-A00

SYSTEMS

SVC

6

-

2A

ALL

80-10-02-160-001-A01

SYSTEMS

SVC

6

Clean Start Control Valve Filter

Applicable to Post SB 145-80-0003 Only.

-

C

ALL

Descripción / Description

Efectividad Effect.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1- 1 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

32-10-00-210-801-A00

STRUCTURAL

GVI

-

-

5000 FC

ALL

32-10-00-220-801-A00

STRUCTURAL

DET

-

-

2500 FC

ALL

32-20-00-210-801-A00

STRUCTURAL

GVI

-

-

5000 FC

ALL

32-20-00-210-802-A00

STRUCTURAL

GVI

-

-

5000 FC

ALL

32-20-00-210-803-A00

STRUCTURAL

GVI

-

-

5000 FC

ALL

32-20-00-210-804-A00

STRUCTURAL

GVI

-

-

5000 FC

ALL

32-20-00-210-805-A00

STRUCTURAL

GVI

-

-

5000 FC

ALL

32-20-00-210-806-A00

STRUCTURAL

GVI

-

-

2500 FC

ALL

32-20-00-220-801-A00

STRUCTURAL

DET

-

-

2500 FC

ALL

52-10-00-220-801-A00

STRUCTURAL

DET

-

Internally inspect the MAIN DOOR (STANDARD MODEL) components: • Only aircraft equipped with STANDARD MAIN Main door folding flap stops (SSI 52-10-04) NOTE: During this inspection, DOOR model. the CPCP basic task shall also be performed for this SSI.

-

5000 FC

ALL

52-10-00-220-801-A01

STRUCTURAL

DET

-

Internally inspect the MAIN DOOR (SIDE-HINGED MODEL) components: • Main door folding flap stops (SSI 52-10-04) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

-

5000 FC

ALL

52-10-00-220-802-A01

STRUCTURAL

DET

-

-

10000 FC

ALL

52-10-00-220-805-A01

STRUCTURAL

DET

-

-

4447 FC

ALL

52-10-00-220-806-A00

STRUCTURAL

DET

-

-

10000 FC

ALL

52-10-00-220-806-A01

STRUCTURAL

DET

-

-

4447 FC

ALL

52-10-00-220-807-A00

STRUCTURAL

DET

-

-

5000 FC

ALL

52-10-00-220-807-A01

STRUCTURAL

DET

-

-

10000 FC

ALL

52-10-00-220-808-A00

STRUCTURAL

DET

-

-

5000 FC

ALL

52-10-00-220-808-A01

STRUCTURAL

DET

-

Externally inspect the MAIN DOOR (SIDE-HINGED MODEL) components: • Stop & backup structures (SSI 52-10-03)

30000

2502 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

52-10-00-220-809-A00

STRUCTURAL

DET

-

Externally inspect the MAIN DOOR (STANDARD MODEL) components: • Stop & backup structures (SSI 52-10-03)

30000

2502 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

52-10-00-220-809-A01

STRUCTURAL

DET

-

Internally inspect the MAIN DOOR (SIDE-HINGED MODEL) components: • Stop & backup structures (SSI 52-10-03)

30000

4447 FC

EMB-145EP; EMB-145ER; MB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

Descripción / Description Externally inspect the MAIN LANDING GEAR components: • Trailing arm MLG (SSI 32-10-03) Externally inspect the MAIN LANDING GEAR components: • Wheel axle MLG (SSI 32-10-04) Externally inspect the NOSE LANDING GEAR components: • Strut (main fitting) - NLG (SSI 32-20-12) Externally inspect the NOSE LANDING GEAR components: • Auxiliary Drag Strut Bottom stay (SSI 32-20-16) Externally inspect the NOSE LANDING GEAR components: • Main Drag Strut Top stay - NLG (SSI 32-20-13) Externally inspect the NOSE LANDING GEAR components: • Auxiliary Drag Strut Top stay (SSI 32-20-15) Externally inspect the NOSE LANDING GEAR components: • Torque links -NLG (SSI 32-20-17) Externally inspect the NOSE LANDING GEAR components: • Sliding tube -NLG (SSI 32-20-18)+D733 Externally inspect the NOSE LANDING GEAR components: • Wheel axle (SSI 32-20-19)

Only aircraft equipped with SIDE HINGED MAIN DOOR model.

Only aircraft equipped with SIDE HINGED Internally inspect the MAIN DOOR (SIDE-HINGED MODEL) components: MAIN DOR model. • Main door folding flap structure (SSI 52-10-02) Only aircraft equipped with SIDE HINGED Internally inspect the MAIN DOOR (SIDE-HINGED MODEL) components: MAIN DOR model. • Main door structure (SSI 52-10-01) Internally inspect the MAIN DOOR (STANDARD MODEL) components: • Only aircraft equipped with STANDARD MAIN DOOR model. Main door folding flap structure (SSI 52-10-02) Only aircraft equipped with SIDE HINGED Externally inspect the MAIN DOOR (SIDE-HINGED MODEL) MAIN DOR model. components: • Main door structure (SSI 52-10-01) Internally inspect the MAIN DOOR (STANDARD MODEL) components: • Only aircraft equipped with STANDARD MAIN DOOR model. Main door structure (SSI 52-10-01) Only aircraft equipped with SIDE HINGED Externally inspect the MAIN DOOR (SIDE-HINGED MODEL) MAIN DOR model. components: • Main door folding flap structures (SSI 52-10-02) Externally inspect the MAIN DOOR (STANDARD MODEL) components: • Only aircraft equipped with STANDARD MAIN DOOR model. Main door folding flap structures (SSI 52-10-02)

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1- 2 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

52-10-00-220-810-A00

STRUCTURAL

DET

-

Internally inspect the MAIN DOOR (STANDARD MODEL) components: • Stop & backup structures (SSI 52-10-03)

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

52-10-00-220-811-A00

STRUCTURAL

DET

-

Externally inspect the MAIN DOOR (STANDARD MODEL) components: • Attachment fittings-to-fuselage & interface parts (SSI 52-10-05)

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

52-10-00-220-812-A00

STRUCTURAL

DET

-

Internally inspect the MAIN DOOR (STANDARD MODEL) components: • Attachment fittings-to-fuselage & interface parts (SSI 52-10-05)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

52-21-00-220-804-A00

STRUCTURAL

DET

-

Externally inspect the PASSENGER CABIN ESCAPE HATCH components: • Escape hatch structure (SSI 52-21-06)

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

52-21-00-220-805-A00

STRUCTURAL

DET

-

Internally inspect the PASSENGER CABIN ESCAPE HATCH components: • Escape hatch structure (SSI 52-21-06)

30000

5060 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

52-21-00-220-806-A00

STRUCTURAL

DET

-

Internally inspect the PASSENGER CABIN ESCAPE HATCH components: • Escape hatch window frame (SSI 52-21-07)

30000

6060 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

52-30-00-220-802-A00

STRUCTURAL

DET

-

Internally inspect the BAGGAGE DOOR components: • Baggage door stops and fittings (SSI 52-30-09)

30000

4318 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

52-43-00-210-801-A00

STRUCTURAL

GVI

-

Internally inspect the SERVICE DOOR components: • Service door folding flap structure (SSI 52-43-11)

-

10000 FC

ALL

52-43-00-210-802-A00

STRUCTURAL

GVI

10000 FC

ALL

52-43-00-220-801-A00

STRUCTURAL

DET

-

-

5000 FC

ALL

52-43-00-220-803-A00

STRUCTURAL

DET

-

Internally inspect the SERVICE DOOR components: • Service door window frame (SSI 52-43-12)

-

5000 FC

ALL

52-43-00-220-807-A00

STRUCTURAL

DET

-

Externally inspect the SERVICE DOOR components: • Service door stops & backup structure (SSI 52-43-13)

22000

2465 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

52-43-00-220-808-A00

STRUCTURAL

DET

-

Internally inspect the SERVICE DOOR components: • Service door stops & backup structure (SSI 52-43-13) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

22000

4640 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

52-43-00-220-809-A00

STRUCTURAL

DET

-

Externally inspect the SERVICE DOOR components: • Service door folding flap stops (SSI 52-43-14)

30000

4975 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

52-43-00-220-810-A00

STRUCTURAL

DET

-

Internally inspect the SERVICE DOOR components: • Service door folding flap stops (SSI 52-43-14) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

Descripción / Description

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

Externally inspect the SERVICE DOOR Service door folding flap structure (SSI 52-43-11) components: Externally inspect the SERVICE DOOR components: • Service door window frame (SSI 52-43-12) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1- 3 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

52-44-00-220-801-A00

STRUCTURAL

DET

-

52-44-00-220-802-A00

STRUCTURAL

DET

-

53-11-00-220-803-A00

STRUCTURAL

DET

-

53-11-00-220-804-A00

STRUCTURAL

DET

-

53-11-00-220-805-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Frames (SSI 53-10-43) Externally inspect the FUSELAGE components: •Fuselage skin panels at Applicable to Aircraft Pre Mod SB 145-53-0067 22000 FC stringers, frames/bulkheads and splices (SSI 53-10-07)

53-12-00-210-801-A00

STRUCTURAL

GVI

-

53-12-00-220-802-A00

STRUCTURAL

DET

-

53-12-00-220-803-A00

STRUCTURAL

DET

-

53-12-00-220-804-A00

STRUCTURAL

DET

-

53-12-00-220-806-A00

STRUCTURAL

DET

-

53-12-00-220-807-A00

STRUCTURAL

DET

-

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

12000 FC

10000 FC

ALL

12000 FC

10000 FC

ALL

Internally inspect the FUSELAGE component: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-10-07)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

Internally inspect the FUSELAGE components: • Forward pressure bulkhead (SSI 53-10-26)

24000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

19737 FC

ALL

328 FC

ALL

5896 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

5896 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

6666 FC

ALL

-

6666 FC

ALL

18000 FC

10000 FC

ALL

4000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

Descripción / Description Externally inspect the REAR ELECTRONIC COMPARTMENT DOOR components: • Rear electronic compartment door structure (SSI 52-4401) Internally inspect the REAR ELECTRONIC COMPARTMENT DOOR components: • Rear electronic compartment door structure (SSI 52-4401)

Internally inspect the FUSELAGE components: • Windshield cutout structure (SSI 53-10-17)

Internally inspect the FUSELAGE components: • Windshield center post, including its attachment and lower fitting (SSI 53-10-19)

Internally inspect the FUSELAGE components: • Cockpit window cutout structure (SSI 53-10-18) Internally inspect the FUSELAGE components: • Cockpit window rear post and its attachment (SSI 53-10-22) Internally inspect the FUSELAGE components: • Forward pressure bulkhead (SSI 53-10-26)

10000 FC

53-12-00-220-808-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Windshield center post, NOTE: Applicable to aircraft Pre-Mod. SB 14512000 FC including its attachments and lower fitting (SSI 53-10-19) 53-0007.

53-12-00-220-809-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Cockpit floor beams and columns (SSI 53-10-27)

-

10000 FC

ALL

53-12-00-220-810-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Windshield cutout structure (SSI 53-10-17)

20000 FC

5896 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

53-12-00-220-811-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Frames (SSI 53-10-43)

-

10000 FC

ALL

Internally inspect the FUSELAGE components: • Forward Pressure Bulkhead (SSI 53-10-26)

18000 FC

9933 FC

ALL

10000 FC

ALL

53-12-00-220-815-A00

STRUCTURAL

DET

-

53-12-00-220-816-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Fuselage skin panel at NOTE: Applicable to aircraft Post-Mod. SB 14553-0051 or Post-Mod. SB 145-53-0067. stringers, frames/bulkheads, and splices (SSI 53-10-07)

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1- 4 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

53-12-00-220-817-A00

STRUCTURAL

DET

-

53-12-00-220-818-A00

STRUCTURAL

DET

-

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

Internally inspect the FUSELAGE components: • Windshield lateral post and its attachment (SSI 53-10-20)

30000

6666 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

Internally inspect the FUSELAGE components: • Windshield center post, including its attachments and lower fitting (SSI 53-10-19) NOTE: Applicable to aircraft Post -Mod. SB 145-53-0007.

26000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

20000 FC

2672 FC

ALL

30000 FC

ALL

-

10000 FC

ALL

-

10000 FC

ALL

Descripción / Description

For aircraft, pre-mod SB 145-53-0058, accumulable between 18,000FC and 20,000 FC or with fatigue threshold exceed perform task 53-12-00-250-801-A00 (insp 1 21,336FC)(insp 2 22,336FC) For aircraft, pre-mod SB 145-53-0058, accumulable between 18,000FC and 20,000 FC or with fatigue threshold exceed perform task 53-12-00-250-801-A00 (insp 1 21,336FC)(insp 2 22,336FC)

53-12-00-250-801-A00

STRUCTURAL

SDE

New MRB task covering SSI 53-10-19 Pre-Mod SB145-53-0058 special detailed inspection, internal side, zone 223/224

53-12-00-250-801-A01

STRUCTURAL

SDE

New MRB task covering SSI 53-10-19, post-mod SB145-53-0058, special detailed inspection, internal side zone 223/224

53-21-00-210-805-A00

STRUCTURAL

GVI

-

53-21-00-210-806-A00

STRUCTURAL

GVI

-

53-21-00-210-811-A00

STRUCTURAL

GVI

-

Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07)

29000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-21-00-220-805-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07)

10000 FC

9816 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

53-21-00-220-806-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Frame 15 & 18 LHS splices at stringers 3L & 16L (SSI 53-20-12)

30000

2979 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

12000 FC

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

5000 FC

ALL

-

5000 FC

ALL

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

Internally inspect the FUSELAGE components: • Main door attachment fittings and interface parts (SSI 53-20-04) Internally inspect the FUSELAGE components: • Service door attachment fittings and interface parts (SSI 53-20-05)

53-21-00-220-807-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Service door cutout reinforcing structure (SSI 53-20-10)

53-21-00-220-811-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Fuselage skin longitudinal splices along main door cutout (SSI 53-20-41)

53-21-00-220-812-A00

STRUCTURAL

DET

-

53-21-00-220-813-A00

STRUCTURAL

DET

-

53-21-00-220-815-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Fuselage skin longitudinal splices along service door cutout (SSI 53-20-42) Externally inspect the FUSELAGE components: • Stops and backup structures for service door (SSI 53-20-02) Externally inspect the FUSELAGE components: • Passenger door cutout reinforcing structure (SSI 53-20-09)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

NOTE: Remove the bumper plate, if installed

13000 FC

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1- 5 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

53-21-00-220-819-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Passenger door cutout reinforcing structures (SSI 53-20-09)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

10000 FC

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

53-21-00-220-820-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Service door cutout reinforcing structures (SSI 53-20-10)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

10000 FC

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

53-21-00-220-823-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Stringer 6 & 16 splices at frames 20 & 22 (SSI 53-20-13)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

30000

2979 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-21-00-220-824-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage skin longitudinal splice (SSI 53-20-08)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

20000 FC

10000 FC

ALL

53-21-00-220-825-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage panel at stringers, frames/bulkheads, and splices (SSI 53-20-07)

20000 FC

9816 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

53-21-00-220-826-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Frames (SSI 53-20-43)

18000 FC

10000 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

53-21-00-220-827-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage skin longitudinal splice (SSI 53-20-08)

20000 FC

10000 FC

ALL

53-21-00-220-839-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Fuselage skin panel and stringers frames/bulkheads and splices (SSI 53-20-07)

-

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

53-21-00-220-842-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Frames (SSI 53-20-43)

18000 FC

9816 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

53-21-00-220-846-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Stops and backup structures for main door (SSI 53-20-01)

25000

3735 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-21-00-220-847-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Stops and backup structure for main door (SSI 53-20-01) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

25000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-21-00-220-848-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Passenger cabin window frame (SSI 53-20-06)

30000

2500 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-21-00-220-849-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Passenger cabin window frame (SSI 53-20-06) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-21-00-220-850-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Frames 15 & 18 LHS splices at stringers 3L & 16L (SSI 53-20-12)

30000

2764 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

Descripción / Description

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1- 6 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

53-21-00-220-851-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Stringers 6 & 16 splices at frames 20 & 22 (SSI 53-20-13)

30000

2764 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-21-00-220-852-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage skin longitudinal splices along main door cutout (SSI 53-20-41) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

30000

4932 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

Descripción / Description

53-21-00-220-853-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage skin longitudinal splices along service door cutout (SSI 53-20-42) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

53-22-00-210-805-A00

STRUCTURAL

GVI

-

Externally inspect the FUSELAGE components: • Fuselage skin panel at stringer, frames/bulkheads, and splices (SSI 53-20-07)

30000

2500 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB145EU; EMB-145EP; EMB-145ER

53-22-00-220-802-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage skin circumferential splice (SSI 53-20-14)

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

53-22-00-220-803-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Frames (SSI 53-20-43)

-

10000 FC

ALL

53-22-00-220-806-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07)

30000

10000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB145EU; EMB-145EP; EMB-145ER

53-23-00-210-802-A00

STRUCTURAL

GVI

-

Internally inspect the FUSELAGE components: • Overwing fuselage skin NOTE: During this inspection, the CPCP basic panel (SSI 53-20-16) task shall also be performed for this SSI.

-

10000 FC

ALL

53-23-00-210-805-A00

STRUCTURAL

GVI

-

Externally inspect the FUSELAGE components: • Overwing fuselage skin panel (SSI 53-20-16)

-

9167 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

53-23-00-210-807-A00

STRUCTURAL

GVI

-

30000

4940 FC

53-23-00-210-808-A00

STRUCTURAL

GVI

53-23-00-210-809-A00

STRUCTURAL

GVI

53-23-00-220-804-A00

STRUCTURAL

DET

-

53-23-00-220-805-A00

STRUCTURAL

DET

-

53-23-00-220-807-A00

STRUCTURAL

DET

-

53-23-00-220-808-A00

STRUCTURAL

DET

-

53-23-00-220-818-A00

STRUCTURAL

DET

-

53-23-00-220-819-A00

STRUCTURAL

DET

-

53-23-00-220-819-A01

STRUCTURAL

DET

-

53-23-00-220-820-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07) Externally inspect the FUSELAGE components: Overwing Fuselage skin panel (SSI 53-20-16) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07)

10000 FC Applicable to aircraft Pre-Mod. SB 145-000032.

Internally inspect the FUSELAGE components: • Frames (SSI 53-20-43) Externally inspect the FUSELAGE components: • Skin and reinforcement around escape hatch cutout (SSI 53-20-51) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07) Internally inspect the FUSELAGE components: • Fuselage machined bulkhead (SSI 53-20-30) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07) Externally inspect the FUSELAGE components: • Skin and reinforcement around escape hatch cutout (SSI 53-20-51) Externally inspect the FUSELAGE components: •Skin and reinforcement around escape cutout reinforcement (SSI 53-20-51) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07)

Applicable to aircraft Post-Mod. SB 145-000032, under ANAC/FAA Certifications. Applicable to aircraft Pre-Mod. SB 145-000032. Applicable to aircraft Post-Mod. SB 145-000032 under ANAC/FAA Certifications.

30000

3388 FC

-

10000 FC

-

5000 FC

30000

10000 FC

30000

10000 FC

18790

2571 FC

-

4725 FC

-

3670 FC

30000

6140 FC

EMB-145EU; EMB-145EP; EMB-145ER EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR ALL EMB-145EU; EMB-145EP; EMB-145ER; EMB-145XR EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR EMB-145EP; EMB-145ER; EMB-145EU F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1- 7 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

53-23-00-220-821-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07)

30000

20000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-23-00-220-822-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-23-00-220-823-A00

STRUCTURAL

DET

-

30000

10000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-23-00-220-824-A00

STRUCTURAL

DET

-

30000

9167 FC

EMB-145EP; EMB-145ER; EMB-145EU

53-23-00-220-825-A00

STRUCTURAL

DET

-

30000

9443 FC

EMB-145EP; EMB-145ER; EMB-145EU

53-24-00-210-801-A00

STRUCTURAL

GVI

-

Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07)

30000

5000 FC

EMB-145EP; EMB-145EU; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

Not applicable to aircrafts model MP

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

Applicable to A/C Pre Mod 145-00-0032

30000

9521 FC

Applicable to aircraft Post-Mod. SB 145-000032, under ANAC/FAA Certifications.

30000

5337 FC

-

9521 FC

-

5732 FC

EMB-145EU; EMB-145EP; EMB-145ER

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU

-

10000 FC

ALL

30000

5000 FC

EMB-145ER; EMB-145EU; EMB-145EP

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

Descripción / Description

Internally inspect the FUSELAGE components: • Fuselage machined bulkhead (SSI 53-20-30) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. Internally inspect the FUSELAGE components: • Fuselage machined bulkhead (SSI 53-20-30) NOTE: During this inspection, the CPCP basic Task shall also be performed for this SSI. Internally inspect the FUSELAGE components: • Fuselage machined bulkhead (SSI 53-20-30)

53-24-00-210-804-A00

STRUCTURAL

GVI

-

Internally inspect the FUSELAGE components: • Fuselage skin circumferential splice (SSI 53-20-14)

53-24-00-210-811-A00

STRUCTURAL

GVI

-

Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices.(SSI 53-20-07)

53-24-00-220-802-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Frames (SSI 53-20-43)

53-24-00-220-806-A00

STRUCTURAL

DET

-

53-24-00-220-806-A01

STRUCTURAL

DET

-

53-24-00-220-807-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07) Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07) Internally inspect the FUSELAGE components: • Frames (SSI 53-20-43) Internally inspect the FUSELAGE components: • Fuselage skin longitudinal splice (SSI 53-20-08) Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07)

53-24-00-220-808-A00

STRUCTURAL

DET

-

53-24-00-220-810-A00

STRUCTURAL

DET

-

53-31-00-210-807-A00

STRUCTURAL

GVI

-

Externally inspect the FUSELAGE components: • Fuselage to vertical stabilizer spar attachment fitting (SSI 53-30-38) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

53-31-00-210-808-A00

STRUCTURAL

GVI

-

Externally inspect the FUSELAGE components: • Fuselage skin panel at pressure bulkhead (SSI 53-30-15)

-

Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-30-07)

53-31-00-210-809-A00

STRUCTURAL

GVI

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

-

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1- 8 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

53-31-00-210-810-A00

STRUCTURAL

GVI

-

Internally inspect the FUSELAGE components: • Baggage compartment floor beams and columns (SSI 53-30-28)

14000

8416 FC

53-31-00-210-811-A00

STRUCTURAL

GVI

-

Externally inspect the FUSELAGE components: • Fuselage skin panel at pressure bulkhead (SSI 53-30-15)

30000

5000 FC

53-31-00-210-821-A00

STRUCTURAL

GVI

-

Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-30-07)

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-31-00-210-822-A00

STRUCTURAL

GVI

-

Externally inspect the FUSELAGE components: • Fuselage skin panel at pressure bulkhead (SSI 53-30-15)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-31-00-210-823-A00

STRUCTURAL

GVI

-

Externally inspect the FUSELAGE components: • Fuselage machined bulkhead (SSI 53-30-30)

30000

10000 FC

EMB-145EP; EMB-145EU; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-31-00-220-803-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Frames (SSI 53-30-43)

-

10000 FC

ALL

-

9199 FC

EMB-145EU; EMB-145EP; EMB-145ER EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-145XR; EMB-145ER; EMB-145EU; EMB-145EP

Descripción / Description

Efectividad Effect. EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

53-31-00-220-807-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Baggage door lateral Lshape. (SSI 53-30-03).

53-31-00-220-808-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Baggage door cutout structure (SSI 53-30-48).

-

2500 FC

53-31-00-220-809-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Rear electronic compartment door cutout structure (SSI 53-30-49).

12000 FC

10000 FC

53-31-00-220-810-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Baggage door lateral Lshape (SSI 53-30-03)

-

7093 FC

53-31-00-220-816-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Baggage door cutout structure (SSI 53-30-48)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

30000

7091 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

53-31-00-220-818-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Rear electronic compartment door cutout structure (SSI 53-30-49)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

12000 FC

7342 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

53-31-00-220-819-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-30-07)

NOTE: Remove bumper plate, if installed.

-

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

53-31-00-220-821-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Baggage door cutout structure (SSI 53-30-48)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

30000

9199 FC

EMB-145ER; EMB-145EU; EMB-145EP

53-31-00-220-822-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Rear electronic compartment door cutout structure (SSI 53-30-49) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

12000 FC

8193 FC

EMB-145ER; EMB-145EU; EMB-145EP

53-31-00-220-840-A00

STRUCTURAL

DET

-

12000 FC

8101 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

53-31-00-220-844-A00

STRUCTURAL

DET

-

-

5700 FC

EMB-145ER; EMB-145EU; EMB-145EP

Externally inspect the FUSELAGE components: • Rear electronic compartment door cutout structure (SSI 53-30-49) Internally inspect the FUSELAGE components: • Fuselage skin longitudinal splice (SSI 53-30-08)

EMB-145EP; EMB-145ER; EMB-145EU EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1- 9 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

53-31-00-220-846-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-30-07)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-31-00-220-847-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-30-07) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-31-00-220-848-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage skin panel at pressure bulkhead (SSI 53-30-15)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-31-00-220-849-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage machined bulkhead (SSI 53-30-30)

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-31-00-220-850-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage machined bulkhead (SSI 53-30-30)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-31-00-220-851-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Bulkhead-to-engine pylon attachment (SSI 53-30-35) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

27000

6256 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-31-00-220-852-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Rear pressure bulkhead (SSI 53-30-36) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

30000

8778 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-31-00-220-852-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage to vertical stabilizer spar attachment fitting (SSI 53-30-38)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-31-00-220-854-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Frames (SSI 53-30-43)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU

Descripción / Description

53-31-00-220-855-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Frames (SSI 53-30-43)

20200

10000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-32-00-210-801-A00

STRUCTURAL

GVI

-

Internally inspect the FUSELAGE components: • APU mounting (SSI 5330-40)

-

20000 FC

ALL

53-32-00-220-810-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage machined bulkhead (SSI 53-30-30)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-32-00-220-811-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage to vertical stabilizer spar attachment fitting (SSI 53-30-38)

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-32-00-220-812-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Tail cone access door cutout structure (SSI 53-30-50)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

53-32-00-220-813-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Tail cone access door cutout structure (SSI 53-30-50)

30000

8193 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-10 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Descripción / Description

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

54-50-00-210-801-A00

STRUCTURAL

GVI

-

Externally inspect the PYLON components: • Pylon Skin (SSI 54-50-04)

18000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB135ER; EMB-135LR; EMB-135KE; EMB135KL

54-50-00-220-802-A00

STRUCTURAL

DET

-

Internally inspect the PYLON components: • FWD engine mounts including bolts (SSI 54-50-03) NOTE: Applicable to aircraft Pre-Mod. SB 145-54-0011.

20000 FC

4000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

54-50-00-220-803-A00

STRUCTURAL

DET

-

Internally inspect the PYLON components: • Pylon Skin (SSI 54-50-04)

18000 FC

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

4000 FC

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

54-50-00-220-808-A00

STRUCTURAL

DET

-

Internally inspect the PYLON components: • AFT Engine Mounts including bolts (SSI 54-50-07) NOTE: Applicable to aircraft Pre-Mod. SB 145-540011.

54-50-00-220-808-A01

STRUCTURAL

DET

-

Internally inspect the PYLON components: • AFT Engine Mounts including bolts (SSI 54-50-07) NOTE: Applicable to aircraft Post-Mod. SB 145-54-0011, and the flight cycles accumulated shall be based on the engine mount components.

5000

5000 FC

54-50-00-220-810-A00

STRUCTURAL

DET

Internally inspect the PYLON components: •Pylon Yokes III and IV (SSI 54-50-02)

30000

4090 FC

54-50-00-220-810-A01

STRUCTURAL

DET

Internally inspect the PYLON components: • Pylon Yokes III and IV (SSI 54-50-02) NOTE: Applicable to aircraft Post-Mod. SB 145-54-0011.

30000

30000 FC

54-50-00-220-812-A00

STRUCTURAL

DET

-

Internally inspect the PYLON components: •Pylon Yokes I and II (SSI 5450-05)

30000

30000 FC

54-50-00-220-813-A00

STRUCTURAL

DET

-

Internally inspect the PYLON components: • Pylon spars I, II, III and IV (SSI 54-50-01) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

27000

5000 FC

54-50-00-230-802-A00

STRUCTURAL

SDE

-

Internally inspect the PYLON components by Liquid Penetrant Inspection Method: • FWD Engine Mounts including bolts (SSI 54-50-03) NOTE: Applicable to aircraft Post-Mod. SB 145-54-0011, and the flight cycles accumulated shall be based on the engine mount c

54-50-00-250-802-A00

STRUCTURAL

SDE

-

Internally inspect the PYLON components by the Eddy Current method: • NOTE: Applicable to aircraft Pre-Mod SB145Pylon Yokes I and II upper flange (SSI 54-50-06) 54-8

15000

15000 FC

30000 FC

6333 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB135ER; EMB-135LR; EMB-135KE; EMB135KL EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB135ER; EMB-135LR; EMB-135KE; EMB135KL EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB135ER; EMB-135LR; EMB-135KE; EMB135KL EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB135ER; EMB-135LR; EMB-135KE; EMB135KL EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB135ER; EMB-135LR; EMB-135KE; EMB135KL EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB135ER; EMB-135LR; EMB-135KE; EMB135KL EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB135ER; EMB-135LR; EMB-135KE; EMB135KL F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-11 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Descripción / Description

Umbral Thrsld.

54-50-00-250-802-A01

STRUCTURAL

SDE

-

Internally inspect the PYLON components by the Eddy Current method: • NOTE: Applicable to aircraft Post-Mod SB145Pylon Yokes I and II upper flange (SSI 54-50-06) 54-0008

54-50-00-250-804-A00

STRUCTURAL

SDE

-

Internally inspect the PYLON components by the Eddy Current method: • Pylon Yokes I and II (SSI 54-50-05) NOTE: Applicable to aircraft PostMod. SB 145-54-0011.

55-10-00-210-803-A00

STRUCTURAL

GVI

-

55-10-00-210-804-A00

STRUCTURAL

GVI

-

55-10-00-210-805-A00

STRUCTURAL

GVI

-

55-10-00-210-806-A00

STRUCTURAL

GVI

Intervalo Interval

Efectividad Effect. EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB135ER; EMB-135LR; EMB-135KE; EMB135KL EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB135ER; EMB-135LR; EMB-135KE; EMB135KL

30000 FC

12606 FC

30000

30000 FC

-

2500 FC

ALL

-

2500 FC

ALL

Externally inspect the HORIZONTAL STABILIZER components: • Skin, from fin to sta. YH = 350 - lower surface (SSI 55-10-06)

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

-

Externally inspect the HORIZONTAL STABILIZER components: • Skin, from rib sta. YH = 350 to rib sta. YH = 990 -upper surface (SSI 55-10-07)

-

10000 FC

ALL

Externally inspect the HORIZONTAL STABILIZER component: • Elevator support fittings (SSI 55-10-15)

-

9635 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

10000 FC

ALL

-

10000 FC

ALL

-

10000 FC

ALL

Externally inspect the HORIZONTAL STABILIZER component: • Fitting hinge support stabilizer (SSI 55-10-21) Internally inspect the HORIZONTAL STABILIZER component: • Pin internal and external hinge stabilizer (SSI 55-10-24)

55-10-00-220-801-A00

STRUCTURAL

DET

-

55-10-00-220-802-A00

STRUCTURAL

DET

-

55-10-00-220-803-A00

STRUCTURAL

DET

-

55-10-00-220-804-A00

STRUCTURAL

DET

-

55-10-00-220-806-A00

STRUCTURAL

DET

-

Internally inspect the HORIZONTAL STABILIZER components: • Skin splice at upper and lower surface (SSI 55-10-16)

Applicable to aircraft Pre-Mod SB 145-550005" (Not applicable Aerolitoral ERJ145 fleet)

-

4227 FC

EMB-145ER; EMB-145EU; EMB-145EP

55-10-00-220-806-A01

STRUCTURAL

DET

-

Internally inspect the HORIZONTAL STABILIZER components: • Skin splice at upper and lower surface (SSI 55-10-16) Note: "Applicable to aircraft Post-Mod SB 145-55-0005"

Applicable to aircraft Post-Mod SB 145-550005"

-

10000 FC

EMB-145ER; EMB-145EU; EMB-145EP

Internally inspect the HORIZONTAL STABILIZER components: • Front/Rear auxiliary spar center fitting ( SSI 55-10-19 )

-

3A

EMB-145EU; EMB-145EP; EMB-145ER; EMB-135ER

-

10000 FC

-

10000 FC

-

3A

EMB-145EU; EMB-145EP; EMB-145ER

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER

55-10-00-220-807-A00

STRUCTURAL

DET

-

55-10-00-220-807-A01

STRUCTURAL

DET

-

55-10-00-220-808-A00

STRUCTURAL

DET

-

Externally inspect the HORIZONTAL STABILIZER component: • Fitting hinge support stabilizer (SSI 55-10-21) Internally inspect the HORIZONTAL STABILIZER components: • Rear spar web and cap, from fin to rib sta. YH =350, including center fitting/spar attachment (SSI 55-10-12) Internally inspect the HORIZONTAL STABILIZER components: • Root rib (SSI 55-10-17)

Internally inspect the HORIZONTAL STABILIZER components: • Front/Rear auxiliary spar center fitting (SSI 55-10-19) Internally inspect the HORIZONTAL STABILIZER components: • Front/Rear auxiliary spar center fitting (SSI 55-10-19)

55-10-00-220-809-A00

STRUCTURAL

DET

-

Internally inspect the HORIZONTAL STABILIZER components: • Front spar center fittings ( SSI 55-10-20 )

55-10-00-220-809-A01

STRUCTURAL

DET

-

Internally inspect the HORIZONTAL STABILIZER components: • Front spar center fittings ( SSI 55-10-20 )

(*) NOTE: Applicable to aircraft Pre-Mod. SB 145-55-0005, perform first inspection at 8000 FC, second inspection at 12000 FC, and the subsequent every 3A (Not applicable Aerolitoral fleet) Applicable to aircraft Post-Mod SB 145-550005"

(*) NOTE: Applicable to aircraft Pre-Mod. SB 145-55-0005, perform first inspection at 8000 FC, second inspection at 12000 FC, and the subsequent every 3A (Not Applicable Aerolitoral fleet) Applicable to aircraft Post-Mod. SB 145-550005.

EMB-145EU; EMB-145EP; EMB-145ER; EMB-135ER EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-12 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

55-10-00-220-810-A00

STRUCTURAL

DET

-

55-10-00-220-811-A00

STRUCTURAL

DET

-

55-10-00-220-812-A00

STRUCTURAL

DET

-

55-10-00-220-813-A00

STRUCTURAL

DET

-

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

Internally inspect the HORIZONTAL STABILIZER components: • Front spar center fittings (SSI 55-10-20)

-

10000 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

Externally inspect the HORIZONTAL STABILIZER component: • Skin, from rib sta YH=350 to rib YH= 990 - upper surface (SSI 55-10-02)

-

7120 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

-

10000 FC

ALL

Descripción / Description

Internally inspect the HORIZONTAL STABILIZER components: • Front and rear auxiliary spar webs and caps, including center fitting/ spar attachment (SSI 55-10-11) Internally inspect the HORIZONTAL STABILIZER components: • Pin, internal and external hinge, stabilizer (SSI 55-10-24) Internally inspect the HORIZONTAL STABILIZER components: • Rear spar center fitting ( SSI 55-10-18 )

-

10000 FC

ALL

(*) NOTE: Applicable to aircraft Pre-Mod. SB 145-55-0005, perform first inspection at 8000 FC, second inspection at 12000 FC, and the subsequent every "3A" check

-

3A

EMB-145EU; EMB-145EP; EMB-145ER

Applicable to aircraft Post-Mod. SB 145-550005.

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER

-

5000 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

55-10-00-220-816-A00

STRUCTURAL

DET

-

55-10-00-220-816-A01

STRUCTURAL

DET

-

55-10-00-220-817-A00

STRUCTURAL

DET

-

55-10-00-220-823-A00

STRUCTURAL

DET

-

Externally inspect the HORIZONTAL STABILIZER components: • Skin, from fin to sta. YH=350 - upper surface (SSI 55-10-01)

-

7120 FC

55-10-00-220-831-A00

STRUCTURAL

DET

-

Internally inspect the HORIZONTAL STABILIZER components: • skin Splice at upper and lower surface (SSI 55-10-16)

-

9342 FC

55-10-00-240-801-A00

STRUCTURAL

SDE

-

Externally inspect the HORIZONTAL STABILIZER components by the magnetic particle inspection method: • Pin, internal and external hinge, stabilizer (SSI 55-10-24)

-

17598 FC

55-10-00-240-802-A00

STRUCTURAL

SDE

-

Applicable to aircraft Pre-Mod. SB 145-000032.

-

17598 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

55-10-00-240-802-A01

STRUCTURAL

SDE

-

NOTE: Applicable to aircraft Post-Mod. SB 14500-0032, under ANAC/FAA Certifications.

-

11723 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

-

29600 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145XR; EMB-135ER; EMB-135KE; EMB-135KL; EMB-135LR

Applicable to aircraft Pre-Mod. SB 145-000032.

-

29600 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

Applicable to aircraft Post-Mod. SB 145-000032, under ANAC/FAA Certifications.

-

19811 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

-

2500 FC

ALL

-

2500 FC

ALL

-

10000 FC

ALL

-

10000 FC

ALL

55-10-00-250-801-A00

STRUCTURAL

SDE

-

55-10-00-250-803-A00

STRUCTURAL

SDE

-

55-10-00-250-803-A01

STRUCTURAL

SDE

-

55-20-00-210-801-A00

STRUCTURAL

GVI

-

55-20-00-210-803-A00

STRUCTURAL

GVI

-

55-20-00-220-801-A00

STRUCTURAL

DET

-

55-20-00-220-802-A00

STRUCTURAL

DET

-

Internally inspect the HORIZONTAL STABILIZER components: • Rear spar center fitting (SSI 55-10-18) NOTE: Applicable to aircraft Post-Mod. SB 145-55-0005. Internally inspect the HORIZONTAL STABILIZER components: • Rear spar center fitting (SSI 55-10-18)

Externally inspect the HORIZONTAL STABILIZER components by the magnetic particle inspection method: • Pin, internal and external hinge, stabilizer (SSI 55-10-24) Externally inspect the HORIZONTAL STABILIZER components by the magnetic particle inspection method: • Pin, internal and external hinge, stabilizer (SSI 55-10-24) Externally inspect the HORIZONTAL STABILIZER components by the eddy current inspection method: • Fitting hing support stabilizer (SSI 5510-21) Externally inspect the HORIZONTAL STABILIZER components by the eddy current inspection method: • Fitting hinge support stabilizer (SSI 5510-21) Externally inspect the HORIZONTAL STABILIZER components by the eddy current inspection method: • Fitting hinge support stabilizer (SSI 5510-21) Internally inspect the ELEVATOR components: • Elevator horn mass balance weights and attachments (SSI 55-20-90) Internally inspect the ELEVATOR components: • Tab wheel drive support fittings (SSI 55-20-35) Internally inspect the ELEVATOR components: • Torque tube fittings (SSI 55-20-34) Internally inspect the ELEVATOR components: • Tab wheel drive support fittings (SSI 55-20-35)

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK EMB-145EP; EMB-145ER; EMB-145EU; EMB-145XR; EMB-135ER; EMB-135KE; EMB-135KL; EMB-135LR

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-13 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

55-30-00-210-802-A00

STRUCTURAL

GVI

-

Internally inspect the VERTICAL STABILIZER components:•Spar 2 (web and cap),from fuselage contour line to tip rib sta. ZV=3015(SSI 55-30-67)

-

10000 FC

ALL

55-30-00-210-803-A00

STRUCTURAL

GVI

-

Internally inspect the VERTICAL STABILIZER components: • Fin-tohorizontal stabilizer support actuators, including bolt (SSI 55-30-75)

-

2500 FC

ALL

55-30-00-210-805-A00

STRUCTURAL

GVI

-

Internally inspect the VERTICAL STABILIZER components: • Spar 1 (web and cap), from fuselage contour line to tip rib (SSI 55-30-68)

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

55-30-00-210-806-A00

STRUCTURAL

GVI

-

Internally inspect the VERTICAL STABILIZER components: • Fitting hinge support (SSI 55-30-76)

-

2500 FC

ALL

55-30-00-210-807-A00

STRUCTURAL

GVI

-

Internally inspect the VERTICAL STABILIZER components: • Rear spar actuator support fitting (elevator) (SSI 55-30-77)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

55-30-00-210-808-A00

STRUCTURAL

GVI

-

Internally inspect the VERTICAL STABILIZER components: • PCU support fittings (SSI 55-30-80)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

55-30-00-220-804-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Spar 3 (web and cap), from fuselage contour line to tip rib, including attachment bolts (SSI 55-30-63)

-

10000 FC

ALL

55-30-00-220-808-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-tofuselage attachment fitting to spar 3 (SSI 55-30-54)

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

55-30-00-220-809-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-tofuselage attachment fitting to auxiliary spar 52% (SSI 55-30-55)

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

Descripción / Description

55-30-00-220-810-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-tofuselage attachment fitting to auxiliary spar 41% (SSI 55-30-56)

55-30-00-220-811-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-tofuselage attachment fitting to bulkhead 78 (SSI 55-30-60)

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

55-30-00-220-812-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-tofuselage attachment fitting to bulkhead 79 (SSI 55-30-61)

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

Internally inspect the VERTICAL STABILIZER components: • Fin-tofuselage attachment fitting to bulkhead 80 (SSI 55-30-62)

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

55-30-00-220-813-A00

STRUCTURAL

DET

-

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-14 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

55-30-00-220-817-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-tofuselage attachment fitting to spar 2 (SSI 55-30-57)

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

55-30-00-220-818-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-tofuselage attachment fitting to spar 1 (SSI 55-30-58)

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

55-30-00-220-819-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-tofuselage attachment fitting to bulkhead 77 (SSI 55-30-59)

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

55-30-00-220-820-A00

STRUCTURAL

DET

-

-

10000 FC

ALL

55-30-00-220-821-A00

STRUCTURAL

DET

-

-

10000 FC

ALL

55-30-00-220-822-A00

STRUCTURAL

DET

-

-

10000 FC

ALL

55-30-00-220-833-A00

STRUCTURAL

DET

-

30000

5574 FC

55-30-00-220-833-A01

STRUCTURAL

DET

-

27000

4591 FC

55-30-00-220-834-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-tohorizontal stabilizer attachment fitting to spar 3 (SSI 55-30-50)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

55-30-00-220-835-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-tohorizontal stabilizer attachment fitting to auxiliary spar 52% (SSI 55-3051)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

55-30-00-220-836-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-tohorizontal stabilizer attachment fitting to auxiliary spar 41% (SSI 55-3052)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

55-30-00-220-837-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Spar 1 - tip rib attachment (SSI 55-30-53)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

55-30-00-220-838-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Tip rib (SSI 55-30-69)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

55-30-00-220-839-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-tohorizontal stabilizer support actuators, including bolt (SSI 55-30-75)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

55-30-00-220-840-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fitting hinge support (SSI 55-30-76)

30000

5574 FC

EMB-145EP; EMB-145ER; EMB-145EU

Descripción / Description

Internally inspect the VERTICAL STABILIZER components: • Spar 52% (web and cap), from fuselage contour line to tip rib, including attachment bolts (SSI 55-30-64) Internally inspect the VERTICAL STABILIZER components: • Spar 41% (web and cap), from sta. ZV=2538 to tip rib, including attachment bolts (SSI 55-30-65) Internally inspect the VERTICAL STABILIZER components: • Spar 41% (web and cap), from sta. ZV=1550.5, including attachment bolts (SSI 5530-66) Internally inspect the VERTICAL STABILIZER components: • Fitting hinge support (SSI 55-30-76) Internally inspect the VERTICAL STABILIZER components: • Fitting hinge support (SSI 55-30-76)

Applicable to aircraft Pre-Mod. SB 145-000032. Applicable to aircraft Post-Mod. SB 145-000032, under ANAC/FAA Certifications.

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-15 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

55-30-00-220-841-A00

STRUCTURAL

DET

-

Externally inspect the VERTICAL STABILIZER components: • Rudder hinge fittings (SSI 55-30-78)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

55-30-00-220-842-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Actuator support fittings (rudder) (SSI 55-30-79)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

55-30-00-250-802-A00

STRUCTURAL

SDE

-

Externally inspect the VERTICAL STABILIZER components by the eddy current inspection method: • Fitting hinge support (SSI 55-30-76)

Applicable to aircraft Pre-Mod. SB 145-000032.

30000

29600 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

55-30-00-250-802-A01

STRUCTURAL

SDE

Externally inspect the VERTICAL STABILIZER components by the eddy current inspection method: • Fitting hinge support (SSI 55-30-76)

Applicable to aircraft Post-Mod. SB 145-000032, under ANAC/FAA Certifications.

27000

19811 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

55-30-00-250-803-A00

STRUCTURAL

SDE

Externally inspect the VERTICAL STABILIZER components by the eddy current inspection method: • Fitting hinge support (SSI 55-30-76)

30000

29600 FC

EMB-145EP; EMB-145ER; EMB-145EU

57-10-00-210-802-A00

STRUCTURAL

GVI

-

30000

20000 FC

57-10-00-220-801-A00

STRUCTURAL

DET

-

-

4382 FC

57-10-00-220-802-A00

STRUCTURAL

DET

-

Internally inspect the WING STUB components: • Lower skin - spanwise splice at spar 2, access holes, stringers, integral milled panel & spanwise splice of integral panel (SSI 57-10-01)

-

5000 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-145XR; EMB-135LR; EMB-135KE; EMB-135KL

57-10-00-220-803-A00

STRUCTURAL

DET

-

Externally inspect the WING STUB components: • Spar 1 - Auxiliary cap attachments & auxiliary cap splice at wing attachments (SSI 57-10-05)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. NOTE (2): Applicable to aircraft Pre Mod SB 145-00-0032 under ANAC / FAA certifications

-

5700 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

57-10-00-220-803-A01

STRUCTURAL

DET

-

NOTE 1: During this inspection, the CPCP Externally inspect the WING STUB components: • Spar 1 - Auxiliary cap basic task shall also be performed for this SSI. attachments & auxiliary cap splice at wing attachments (SSI 57-10-05) NOTE 2: Applicable to aircraft Post-Mod. SB 145-00-0032, under ANAC/FAA Certifications.

-

5049 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

-

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

Descripción / Description

Externally inspect the WING STUB components: • Spar 2 - brackets and rib 2A web attachments (SSI 57-10-27) Externally inspect the WING STUB components: • Lower skin - Spanwise NOTE: During this inspection, the CPCP basic splice at spar 2, access holes, stringers, integral milled panels & task shall also be performed for this SSI. spanwise splice of integral panel (SSI 57-10-01)

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR EMB-145ER; EMB-145EU; EMB-145EP; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-10-00-220-804-A00

STRUCTURAL

DET

-

Internally inspect the WING STUB components: • Lower skin - ribs 1, 2 & NOTE: During this inspection, the CPCP basic 3 attachments and tire compartment wall attachments (SSI 57-10-02) task shall also be performed for this SSI.

57-10-00-220-806-A00

STRUCTURAL

DET

-

Externally inspect the WING STUB components: • Lower skin - ribs 1, 2 & NOTE: During this inspection, the CPCP basic 3 attachments and tire compartment wall attachments (SSI 57-10-02) task shall also be performed for this SSI.

-

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-10-00-220-807-A00

STRUCTURAL

DET

-

Externally inspect the WING STUB components: • Spar 1 - lower skin attachments (SSI 57-10-03)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. NOTE(2): applicable to aircraft Pre Mod SB 145-00-0032

-

5700 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

57-10-00-220-807-A01

STRUCTURAL

DET

-

Externally inspect the WING STUB components: • Spar 1 - lower skin attachments (SSI 57-10-03)

NOTE 1:During this inspection, the CPCP basic task shall also be performed for this SSI. NOTE 2: Applicable to aircraft Post-Mod. SB 145-00-0032, under ANAC/FAA Certifications.

-

5049 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-16 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

57-10-00-220-808-A00

STRUCTURAL

DET

-

57-10-00-220-809-A00

STRUCTURAL

DET

-

57-10-00-220-809-A01

STRUCTURAL

DET

57-10-00-220-810-A00

STRUCTURAL

DET

57-10-00-220-810-A01

STRUCTURAL

DET

57-10-00-220-811-A00

STRUCTURAL

DET

-

57-10-00-220-812-A00

STRUCTURAL

DET

-

57-10-00-220-813-A00

STRUCTURAL

DET

-

57-10-00-220-813-A01

STRUCTURAL

DET

-

57-10-00-220-814-A00

STRUCTURAL

DET

-

57-10-00-220-814-A01

STRUCTURAL

DET

57-10-00-220-815-A00

STRUCTURAL

57-10-00-220-816-A00

Descripción / Description Externally inspect the WING STUB components: • Spar 2 - lower skin attachments (SSI 57-10-06) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. Internally inspect the WING STUB components: • Spar 1 - lower skin attachments (SSI 57-10-03) Internally inspect the WING STUB components: • Spar 1 - lower skin attachments (SSI 57-10-03)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. NOTE: Applicable to aircraft Pre Mod SB 14500-0032 Applicable to aircraft Post-Mod. SB 145-000032, under ANAC/FAA Certifications.

Umbral Thrsld.

Intervalo Interval

20000 FC

5000 FC

-

5700 FC

-

5049 FC

Efectividad Effect. EMB-145EP; EMB-145ER; EMB-145EU; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

Internally inspect the WING STUB components: • Spar 1 - Auxiliary cap attachments & auxiliary cap splice at wing attachments (SSI 57-10-05)

NOTE: Applicable to aircraft Pre Mod SB 14500-0032

-

5700 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

Internally inspect the WING STUB components: • Spar 1 - Auxiliary cap attachments & auxiliary cap splice at wing attachments (SSI 57-10-05)

Applicable to aircraft Post-Mod. SB 145-000032, under ANAC/FAA Certifications.

-

5049 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

Internally inspect the WING STUB components: • Spar 2 - lower skin attachments (SSI 57-10-06)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

20000 FC

5852 FC

EMB-145ER; EMB-145EU; EMB-145EP; EMB-135ER

-

5852 FC

EMB-145ER; EMB-145EU; EMB-145EP; EMB-135ER

23000

9583 FC

22000

8759 FC

Internally inspect the WING STUB components: • Spar 2 - Auxiliary cap NOTE: Applicable to aircraft Pre Mod SB 145attachments and auxiliary cap splice at wing attachments (SSI 57-10-08) 00-0032

-

9583 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

-

Internally inspect the WING STUB components: • Spar 2 - Auxiliary cap attachments and auxiliary cap splice at wing attachments (SSI 57-10-08)

-

8759 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

DET

-

Internally inspect the WING STUB components: • Lower skin - Spanwise NOTE: During this inspection, the CPCP basic splice at spar 2, access holes, stringers, integral milled panel & spanwise task shall also be performed for this SSI. splice of integral panel (SSI 57-10-01)

-

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-135ER

STRUCTURAL

DET

-

Internally inspect the WING STUB components: • Spar 1 - Auxiliary cap attachments & auxiliary cap splice at wing attachments (SSI 57-10-05)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

-

4179 FC

57-10-00-220-817-A00

STRUCTURAL

DET

-

Internally inspect the WING STUB components: • Spar 1 - Lower skin attachments (SSI 57-10-03) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

-

4179 FC

57-10-00-220-822-A00

STRUCTURAL

DET

-

Externally inspect the WING STUB components: • Lower skin-spanwise During this inspection, the CPCP basic task splice at spart 2, access holes, stringers, integral milled panels and shall also be performed for this SSI. NOTE(2): spanwise splice of integral panel (SSI 57-10-01) Applicable to aircraft Pre Mod SB 145-00-0032

-

4417 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

57-10-00-220-822-A01

STRUCTURAL

DET

-

NOTE 1: During this inspection, the CPCP Externally inspect the WING STUB components: • Lower skin Spanwise basic task shall also be performed for this SSI. splice at spar 2, access holes, stringers, integral milled panels & NOTE 2: Applicable to aircraft Post-Mod. SB spanwise splice of integral panel (SSI 57-10-01) 145-00-0032, under ANAC/FAA Certifications.

-

3825 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

57-10-00-220-826-A00

STRUCTURAL

DET

-

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

-

4179 FC

57-10-00-220-827-A00

STRUCTURAL

DET

-

Externally inspect the WING STUB components: • Spar 1-auxiliary cap NOTE: During this inspection, the CPCP basic attachments and auxiliary cap splice at wing attachments (SSI 57-10-05). task shall also be performed for this SSI.

-

4179 FC

-

Internally inspect the WING STUB components: • Spar 2 - Auxiliary cap NOTE: During this inspection, the CPCP basic attachments and auxiliary cap splice at wing attachments (SSI 57-10-08) task shall also be performed for this SSI. Internally inspect the WING STUB components: • Spar 2 - Lower skin attachments (SSI 57-10-06) Internally inspect the WING STUB components: • Spar 2 - Lower skin attachments (SSI 57-10-06)

Internally inspect the WING STUB components: • Spar 1-lower skin attachments (SSI 57-10-03).

NOTE: Applicable to aircraft Pre Mod SB 14500-0032 Applicable to aircraft Post-Mod. SB 145-000032, under ANAC/FAA Certifications.

Applicable to aircraft Post-Mod. SB 145-000032, under ANAC/FAA Certifications.

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

EMB-145EU; EMB-145EP; EMB-145ER; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145EU; EMB-145EP; EMB-145ER; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

EMB-145EU; EMB-145EP; EMB-145ER; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145EU; EMB-145EP; EMB-145ER; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-17 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

57-10-00-220-833-A00

STRUCTURAL

DET

-

57-10-00-220-833-A01

STRUCTURAL

DET

-

57-10-00-220-834-A00

STRUCTURAL

DET

-

57-10-00-250-801-A00

STRUCTURAL

SDE

-

57-10-00-250-801-A01

STRUCTURAL

SDE

-

57-11-00-220-808-A00

STRUCTURAL

DET

-

57-11-00-220-814-A00

STRUCTURAL

DET

-

57-11-00-220-831-A00

STRUCTURAL

DET

-

57-11-00-220-839-A00

STRUCTURAL

DET

-

57-11-00-220-840-A00

STRUCTURAL

DET

-

57-11-00-220-841-A00

STRUCTURAL

DET

-

57-11-00-220-842-A00

STRUCTURAL

DET

-

57-11-00-220-843-A00

STRUCTURAL

DET

-

57-11-00-220-844-A00

STRUCTURAL

DET

-

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

Externally inspect the WING STUB components: • Spar 2 - lower skin attachments (SSI 57-10-06) NOTE 1: During this inspection, the CPCP basic task shall also be performed for this SSI. NOTE 2: Applicable to aircraft Pre-Mod. SB 145-00-0032.

23000

5000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

Externally inspect the WING STUB components: • Spar 2 - lower skin attachments (SSI 57-10-06) NOTE 1: During this inspection, the CPCP basic task shall also be performed for this SSI. NOTE 2: Applicable to aircraft Post-Mod. SB 145-00-0032, under ANAC/FAA

22000

5000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

30000

5000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

23600

9569 FC

ALL

24000 FC

ALL

30000

5617 FC

EMB-145EU; EMB-145EP; EMB-145ER

30000

10000 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

30000

10000 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

30000

20000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

30000

20000 FC

EMB-145EP; EMB-145ER; EMB-145EU

30000

5617 FC

EMB-145EP; EMB-145ER; EMB-145EU

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

30000

5000 FC

EMB-145EP; EMB-145ER ;EMB-145EU

Descripción / Description

Internally inspect the WING STUB components: • Spar 2 - brackets and rib 2A web attachments (SSI 57-10-27) Externally inspect the WING STUB components using Eddy Current inspection method: • Rib 4 – lower flange and web (SSI 57-10-11) NOTE: Applicable to aircraft Pre-Mod. SB 145-57-0047. Externally inspect the WING STUB components using Eddy Current inspection method: • Rib 4 – lower flange and web (SSI 57-10-11) NOTE: Applicable to aircraft Post-Mod. SB 145-57-0047. Externally inspect the WING STUB components: • Spar 1 - lower front NOTE: During this inspection, the CPCP basic fitting attachments and spar 2 - lower rear fitting attachments (SSI 57-11task shall also be performed for this SSI. 18) Internally inspect the WING STUB components: • Spar 1 - lower front fitting attachments and spar 2 - lower rear fitting attachments (SSI 57-1118) Externally inspect the WING STUB components: • Spar 1-lower from NOTE: During this inspection, the CPCP basic fitting attachments and spar 2-lower rear fitting attachments (SSI 57-11task shall also be performed for this SSI. 18) Externally inspect the WING STUB components: • Lower skin - rear fittingto-skin attachments and spars 1 & 2 - stub-to-wing attachments (SSI 5711-17) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. Internally inspect the WING STUB components: • Lower skin - rear fittingto-skin attachments and spars 1 & 2 - stub-to-wing attachments (SSI 5711-17) Internally inspect the WING STUB components: • Lower skin - rear fittingto-skin attachments and spars 1 & 2 - stub-to-wing attachments (SSI 5711-17) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. Internally inspect the WING STUB components: • Spar 1 - Lower front fitting attachments and spar 2 - lower rear fitting attachments (SSI 57-1118) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. Externally inspect the WING STUB components: • Spar 1 - Titanium fitting attachments, fuselage bulkhead attachments at frame 40, L - shape fuselage frame 40 attachments & fuselage stringers attachments (SSI 5711-19) NOTE: During this inspection, the CPCP Internally inspect the WING STUB components: • Spar 1 - Titanium fitting attachments, fuselage bulkhead attachments at frame 40, L - shape fuselage frame 40 attachments & fuselage stringers attachments (SSI 5711-19) NOTE: During this inspection, the CPCP

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-18 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

57-11-00-220-845-A00

STRUCTURAL

DET

-

57-11-00-220-846-A00

STRUCTURAL

DET

-

57-11-00-220-847-A00

STRUCTURAL

DET

-

57-11-00-220-848-A00

STRUCTURAL

DET

-

57-11-00-220-849-A00

STRUCTURAL

DET

-

57-11-00-220-850-A00

STRUCTURAL

DET

-

57-11-00-220-851-A00

STRUCTURAL

DET

-

57-11-00-220-852-A00

STRUCTURAL

DET

-

57-11-00-220-853-A00

STRUCTURAL

DET

-

57-11-00-220-854-A00

STRUCTURAL

DET

-

57-11-00-220-855-A00

STRUCTURAL

DET

-

57-11-00-220-856-A00

STRUCTURAL

DET

-

57-11-00-220-857-A00

STRUCTURAL

DET

-

57-11-00-220-858-A00

STRUCTURAL

DET

-

Descripción / Description Internally inspect the WING STUB components: • Spar 1 - Titanium fitting attachments, fuselage bulkhead attachments at frame 40, L - shape fuselage frame 40 attachments & fuselage stringers attachments (SSI 5711-19) Externally inspect the WING STUB components: • Spar 2 -Titanium fitting attachments and fuselage bulkhead attachments at frame 46 (SSI 57-1120) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. Internally inspect the WING STUB components: • Spar 2 - Titanium fitting attachments and fuselage bulkhead at frame 46 (SSI 57-11-20) Internally inspect the WING STUB components: • Spar 2 - Titanium fitting attachments and fuselage bulkhead at frame 46 (SSI 57-11-20) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. Externally inspect the WING STUB components: • Spar 3 - Fuselage bulkhead attachments at frame 50, L - shape fuselage frame 50 attachments & fuselage stringers attachments (SSI 57-11-21) NOTE: During this inspection, the CPCP basic task shall also be perf Externally inspect the WING STUB components: • Spar 3 - Fuselage bulkhead attachments at frame 50, L - shape fuselage frame 50 attachments & fuselage stringers attachments (SSI 57-11-21) NOTE: During this inspection, the CPCP basic task shall also be perf Internally inspect the WING STUB components: • Spar 3 - Fuselage bulkhead attachments at frame 50, L - shape fuselage frame 50 attachments & fuselage stringers attachments (SSI 57-11-21) NOTE: During this inspection, the CPCP basic task shall also be perf Internally inspect the WING STUB components: • Spar 3 - Fuselage bulkhead attachments at frame 50, L - shape fuselage frame 50 attachments & fuselage stringers attachments (SSI 57-11-21) NOTE: During this inspection, the CPCP basic task shall also be perf Externally inspect the WING STUB components: • Spar 3 and rib 4 rodend link (SSI 57-11-22) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. Externally inspect the WING STUB components: • Fuselage bulkhead at frame 40 and its attachments to frame 40 (SSI 57-11-23) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. Externally inspect the WING STUB components: • Fuselage bulkhead at frame 40 and its attachments to frame 40 (SSI 57-11-23) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. Internally inspect the WING STUB components: • Fuselage bulkhead at frame 40 and its attachments to frame 40 (SSI 57-11-23) Internally inspect the WING STUB components: • Fuselage bulkhead at frame 40 and its attachments to frame 40 (SSI 57-11-23) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. Externally inspect the WING STUB components: • Fuselage bulkhead attachments to frame 46 (SSI 57-11-24) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

30000

10000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

30000

5000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU

30000

5000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU

30000

10000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

30000

10000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

30000

9388 FC

EMB-145EP; EMB-145ER; EMB-145EU

30000

10000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

30000

9388 FC

EMB-145EP; EMB-145ER; EMB-145EU

30000

10000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-19 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

57-11-00-220-859-A00

STRUCTURAL

DET

-

Externally inspect the WING STUB components: • Fuselage bulkhead attachments to frame 46 (SSI 57-11-24) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

30000

9047 FC

EMB-145EP; EMB-145ER; EMB-145EU

57-11-00-220-860-A00

STRUCTURAL

DET

-

Internally inspect the WING STUB components: • Fuselage bulkhead attachments to frame 46 (SSI 57-11-24) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

30000

10000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

57-11-00-220-861-A00

STRUCTURAL

DET

-

Internally inspect the WING STUB components: • Fuselage bulkhead attachments to frame 46 (SSI 57-11-24) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

30000

9047 FC

EMB-145EP; EMB-145ER; EMB-145EU

57-11-00-220-862-A00

STRUCTURAL

DET

-

Externally inspect the WING STUB components: • Fuselage bulkhead at frame 50 and its attachments to frame 50 (SSI 57-11-25) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

30000

20000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

57-11-00-220-863-A00

STRUCTURAL

DET

-

Internally inspect the WING STUB components: • Fuselage bulkhead at frame 50 and its attachments to frame 50 (SSI 57-11-25) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

30000

20000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

57-11-00-250-801-A00

STRUCTURAL

SDE

-

Internally inspect the WING STUB components by using Eddy Current Inspection Method: • Lower skin - rear fitting-to-skin attachments and spars 1 & 2 - stub-to-wing attachments (SSI 57-11-17)

-

30000 FC

ALL

57-21-00-210-801-A00

STRUCTURAL

GVI

-

-

2500 FC

ALL

57-21-00-210-804-A00

STRUCTURAL

GVI

-

-

10000 FC

ALL

57-21-00-210-805-A00

STRUCTURAL

GVI

-

-

20000 FC

ALL

57-21-00-210-806-A00

STRUCTURAL

GVI

-

-

5000 FC

ALL

57-21-00-210-807-A00

STRUCTURAL

GVI

-

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-21-00-210-810-A00

STRUCTURAL

GVI

-

-

10000 FC

ALL

57-21-00-210-811-A00

STRUCTURAL

GVI

-

57-21-00-210-812-A00

STRUCTURAL

GVI

-

57-21-00-210-814-A00

STRUCTURAL

GVI

-

57-21-00-210-815-A00

STRUCTURAL

GVI

-

57-21-00-210-816-A00

STRUCTURAL

GVI

57-21-00-210-817-A00

STRUCTURAL

GVI

Descripción / Description

Externally inspect the WING components: • Lower skin/spar attachments (SSI 57-21-36) Internally inspect the WING components: • Lower skin panel spanwise joint (SSI 57-21-30) Internally inspect the WING components: • Lower skin panel chordwise joint (SSI 57-21-29) Internally inspect the WING components: • Lower skin/spar attachments (SSI 57-21-36) Externally inspect the WING components: • Actuator access holes (SSI 57-21-34) Internally inspect the WING components: • Actuator access holes (SSI 5721-34) Internally inspect the WING components: • Lower skin access holes (SSI 57-21-32) Internally inspect the WING components: • Lower skin access holes (SSI 57-21-32) Externally inspect the WING components: • Lower skin panel spanwise joint (SSI 57-21-30) Externally inspect the WING components: • Upper skin panel spanwise joint (SSI 57-21-31)

-

10000 FC

ALL

20000 FC

20000 FC

ALL

-

2500 FC

ALL

-

2500 FC

ALL

-

Externally inspect the WING components: • Upper skin/spar attachments (SSI 57-21-37)

12000 FC

2500 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

Internally inspect the WING components: • Lower skin panel spanwise joint (SSI 57-21-30)

-

20000 FC

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-20 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

57-21-00-210-818-A00

STRUCTURAL

GVI

-

57-21-00-210-819-A00

STRUCTURAL

GVI

57-21-00-210-820-A00

STRUCTURAL

57-21-00-210-826-A00

STRUCTURAL

57-21-00-210-828-A00

STRUCTURAL

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

Internally inspect the WING components: • Lower skin access holes (SSI 57-21-32)

20000 FC

20000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-145XR

-

Internally inspect the WING components: • Skin panels (SSI 57-21-26)

-

5000 FC

GVI

-

Internally inspect the WING components skin panels (SSI 57-21-26)

-

5000 FC

GVI

-

Externally inspect the WING components: • Skin panels (SSI 57-21-26)

-

12888 FC

Descripción / Description

Externally inspect the WING components: Lower Skin access holes (SSI 57-21-32) Externally inspect the WING components: Skin panels (SSI 57-21-26) NOTE: Applicable to aircraft Pre-Mod. SB 145-00-0032.

GVI

EMB-145ER; EMB-145EU; EMB-145EP; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK EMB-145EP; EMB-145ER; EMB-145EU

5000 FC

ALL

18298 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

57-21-00-210-829-A00

STRUCTURAL

GVI

57-21-00-210-830-A00

STRUCTURAL

GVI

Internally inspect the WING components: • Lower skin/spar attachments (SSI 57-21-36)

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

57-21-00-210-832-A00

STRUCTURAL

GVI

Internally inspect the WING components: • Lower skin access holes (SSI 57-21-32)

30000

20000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

57-21-00-210-833-A00

STRUCTURAL

GVI

Externally inspect the WING components: • Lower skin access holes (SSI 57-21-32)

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

Externally inspect the WING components: • Lower vent hole (SSI 57-2133)

57-21-00-210-834-A00

STRUCTURAL

GVI

57-21-00-220-803-A00

STRUCTURAL

DET

10000 FC

-

2500 FC

EMB-145EU; EMB-145EP; ; EMB145ER; EMB-145LR; EMB-145LU; EMB145MR; EMB-145MP; EMB-145MK; ; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145EU; EMB-145EP; EMB-145ER; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

Externally inspect the WING components: • Skin panels (SSI 57-21-26)

12000 FC

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-21-00-220-804-A00

STRUCTURAL

DET

-

Internally inspect the WING components: Upper skin/ spar attachment (SSI 57-21-37)

57-21-00-220-805-A00

STRUCTURAL

DET

-

Externally inspect the WING components: • Skin panels (SSI 57-21-26)

-

2500 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK

57-21-00-220-814-A00

STRUCTURAL

DET

-

Internally inspect the WING components: • Lower skin/spar attachments (SSI 57-21-36)

30000

8099 FC

EMB-145EU; EMB-145EP; EMB-145ER

57-21-00-220-815-A00

STRUCTURAL

DET

-

Externally inspect the WING components: • Lower skin/spar attachments (SSI 57-21-36)

-

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-21-00-220-819-A00

STRUCTURAL

DET

-

Externally Inspect the WING components: • Lower Skin/Spar attachments (SSI 57-21-36)

30000

8444 FC

57-21-00-220-821-A00

STRUCTURAL

DET

-

Externally inspect the WING components: • Skin panels (SSI 57-21-26)

-

11560 FC

Applicable to aircraft Post-Mod. SB 145-000032, under ANAC/FAA Certifications.

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-21 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

57-21-00-250-802-A00

STRUCTURAL

SDE

-

-

17395 FC

57-21-00-250-803-A00

STRUCTURAL

SDE

-

-

17395 FC

57-21-00-250-803-A01

STRUCTURAL

SDE

-

-

11192 FC

57-22-00-210-801-A00

STRUCTURAL

GVI

-

-

10000 FC

ALL

57-22-00-210-806-A00

STRUCTURAL

GVI

-

Internally inspect the WING components: • Spar 1 cap (SSI 57-22-41)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

57-22-00-220-802-A00

STRUCTURAL

DET

-

Externally inspect the WING components: • Spar 1/web cutouts (SSI 5722-42)

-

10000 FC

ALL

57-22-00-220-804-A00

STRUCTURAL

DET

-

Internally inspect the WING components: • Spar 1/leading edge attachments (SSI 57-22-43)

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-22-00-220-808-A00

STRUCTURAL

DET

-

Externally inspect the WING components: • Spar 1/Leading edge attachments (SSI 57-22-43)

-

5000 FC

ALL

57-22-00-220-809-A00

STRUCTURAL

DET

-

Externally inspect the WING components: • Spar 1/web and stiffeners (SSI 57-22-40)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

57-22-00-250-801-A00

STRUCTURAL

SDE

-

Externally inspect the WING components by using Eddy Current Inspection Method: • Spar 1, web cutout (SSI 57-22-42)

-

23895 FC

EMB-145EU; EMB-145EP; EMB-145ER

Descripción / Description Externally inspect the WING components by using Eddy Current method: Lower skin panel chordwise joint (SSI 57-21-29) Externally inspect the WING components by using Eddy Current method: • Lower skin panel chordwise joint (SSI 57-21-29) Externally inspect the WING components by using Eddy Current method: • Lower skin panel chord wise joint (SSI 57-21-29) Internally inspect the WING components: • Spar 1/wing stub attachments (SSI 57-22-44)

Applicable to aircraft Pre-Mod. SB 145-000032. Applicable to aircraft Post-Mod. SB 145-000032, under ANAC/FAA Certifications.

Efectividad Effect. EMB-145EP; EMB-145ER; EMB-145EU; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

57-22-00-250-803-A00

STRUCTURAL

SDE

-

Externally inspect the WING components by Using Eddy Current Inspection Method: • Spar I web cutouts (SSI 57-22-42)

-

16279 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-23-00-210-801-A00

STRUCTURAL

GVI

-

Externally inspect the WING components: • Spar 2/Wing Stub Attachments (SSI 57-23-48)

-

5000 FC

ALL

57-23-00-210-805-A00

STRUCTURAL

GVI

-

Internally inspect the WING components: • Spar 2 cap (SSI 57-23-46)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

57-23-00-220-802-A00

STRUCTURAL

DET

-

-

10000 FC

ALL

57-23-00-220-805-A00

STRUCTURAL

DET

-

-

10000 FC

ALL

57-23-00-220-806-A00

STRUCTURAL

DET

-

Internally inspect the WING components: • Spar 2/web and stiffeners (SSI 57-23-45)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

57-23-00-220-807-A00

STRUCTURAL

DET

-

Internally inspect the WING components: • Spar 2/web cutouts (SSI 5723-47)

30000

10000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

57-24-00-210-802-A00

STRUCTURAL

GVI

-

Externally inspect the WING components: • Spar 3/wing stub attachments (SSI 57-24-52)

-

5000 FC

ALL

Externally inspect the WING components: • Spar 2/web cutouts (SSI 5723-47) Internally inspect the WING components: • Spar 2/web and stiffeners (SSI 57-23-45)

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-22 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

57-24-00-210-803-A00

STRUCTURAL

GVI

-

Internally inspect the WING components: • Spar 3 cap (SSI 57-24-50)

30000

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

57-26-00-220-802-A00

STRUCTURAL

DET

-

Externally inspect the WING components: • FWD & AFT side brace fittings - MLG (SSI 57-26-56)

Applicable to A/C Pre-Mod. SB 145-57-0009.

-

500 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-135ER

57-26-00-220-802-A01

STRUCTURAL

DET

-

Externally inspect the WING components: • FWD & AFT side brace fittings - MLG (SSI 57-26-56)

Applicable to aircraft Pre-Mod. SB 145-570018.

-

2500 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135LR; EMB-135KE; EMB-135KL

57-26-00-220-802-A03

STRUCTURAL

DET

-

Externally inspect the WING components: • FWD & AFT side brace fittings - MLG (SSI 57-26-56)

Applicable to aircraft Post-Mod. SB 145-570009 AND Pre-Mod. SB 145-57-0030.

-

2500 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-135ER

57-26-00-220-802-A04

STRUCTURAL

DET

-

Externally inspect the WING components: • FWD & AFT side brace fittings - MLG (SSI 57-26-56)

Applicable to aircraft Post-Mod. SB 145-570018.

-

5000 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-145XR; EMB-135LR; EMB-135KE; EMB-135KL

57-26-00-220-802-A05

STRUCTURAL

DET

-

Applicable to aircraft Post-Mod. SB 145-570030

-

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-135ER

57-26-00-220-804-A00

STRUCTURAL

DET

-

-

5000 FC

ALL

57-26-00-220-805-A00

STRUCTURAL

DET

-

-

5000 FC

ALL

57-26-00-220-806-A00

STRUCTURAL

DET

-

Externally inspect the WING components: • FWD & AFT side brace fittings - MLG (SSI 57-26-56) Externally inspect the WING components: • Lower bearing cap (SSI 5726-94) Externally inspect the WING components: • AFT upper trunnion (SSI 5726-95) Externally inspect the WING components: • FWD upper trunnion (SSI 5726-96)

-

5000 FC

57-26-00-250-802-A00

STRUCTURAL

SDE

-

57-26-00-250-803-A00

STRUCTURAL

SDE

-

57-26-00-250-809-A00

STRUCTURAL

SDE

-

Descripción / Description

Externally inspect the WING components using Eddy Current Inspection Method: • FWD & AFT side brace fittings (SSI 57-26-56) Externally inspect the WING components using Eddy Current Inspection Method: • Lower bearing cap (SSI 57-26-94) Externally inspect the WIING components using Eddy Current Inspection Method: • Fwd and Aft side brace fittings (SSI 57-26-56) Externally inspect the WING components using Eddy Current Inspection Method: • Lower Bearing Cap (SSI 57-26-94) Externally inspect the WING components using Eddy Current Inspection Method: • Lower Bearing Cap (SSI 57-26-94)

57-26-00-250-812-A00

STRUCTURAL

SDE

-

57-26-00-250-812-A01

STRUCTURAL

SDE

-

57-26-00-250-813-A00

STRUCTURAL

SDE

-

Externally inspect the WING components using Eddy Current inspection method: • Aft upper Trunnion (SSI 57-26-95)

57-26-00-250-813-A01

STRUCTURAL

SDE

-

Externally inspect the WING components using Eddy Current inspection method: • Aft upper Trunnion (SSI 57-26-95)

57-26-00-250-813-A02

STRUCTURAL

SDE

-

57-26-00-250-813-A03

STRUCTURAL

SDE

-

Applicable to aircraft Pre-Mod. SB 145-000032. Applicable to aircraft Post-Mod. SB 145-000032, under ANAC/FAA Certifications. NOTE 1: Applicable only to trunnion P/N 14567014-001/002/003/004/005/006/007/ 008. NOTE 2: Applicable to aircraft Pre-Mod. SB 145-00-0032. NOTE 1: Applicable only to trunnion P/N 14567014-001/002/003/004/005/006/007/ 008. NOTE 2: Applicable to aircraft Post-Mod. SB 145-00-0032, under ANAC/FAA Certifications.

NOTE 1: Applicable only to trunnion P/N 145Externally inspect the WING components using Eddy Current inspection 67014-011/012. NOTE 2: Applicable to aircraft method: • Aft upper Trunnion (SSI 57-26-95) Pre-Mod. SB 145-00-0032. NOTE 1: Applicable only to trunnion P/N 145Externally inspect the WING components using Eddy Current inspection 67014-011/012. NOTE 2: Applicable to aircraft method: • Aft upper Trunnion (SSI 57-26-95) Post-Mod. SB 145-00-0032, under ANAC/FAA Certifications.

-

16399 FC

-

12751 FC

-

30000 FC

ALL EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL; EMB-145XR EMB-145EP; EMB-145ER; EMB-145EU EMB-145EU; EMB-145EP; EMB-145ER EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

-

12751 FC

-

21620 FC

17800

16459 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

12985 FC

11927 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

11000

10413 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

6564 FC

6179 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-23 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

57-26-00-250-813-A04

STRUCTURAL

SDE

-

57-26-00-250-813-A05

STRUCTURAL

SDE

-

57-26-00-250-814-A00

STRUCTURAL

SDE

-

57-26-00-250-814-A01

STRUCTURAL

SDE

-

57-26-00-250-815-A00

STRUCTURAL

SDE

-

57-26-00-250-815-A01

STRUCTURAL

SDE

-

57-26-00-250-815-A02

STRUCTURAL

SDE

-

57-26-00-250-816-A00

STRUCTURAL

SDE

-

57-28-00-210-802-A00

STRUCTURAL

GVI

-

57-28-00-210-803-A00

STRUCTURAL

GVI

-

57-28-00-210-804-A00

STRUCTURAL

GVI

57-28-00-210-805-A00

STRUCTURAL

57-28-00-210-806-A00

Descripción / Description Externally inspect the WING components using Eddy Current inspection method: • Aft upper Trunnion (SSI 57-26-95)

NOTE 1:Applicable only to trunnion P/N 14567014-009/010/013/014. NOTE 2: Applicable to aircraft Pre-Mod.S B 145-00-0032

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

22200

20000 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

15409 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

NOTE 1:Applicable only to trunnion P/N 145Externally inspect the WING components using Eddy Current inspection 67014-009/010/013/014. NOTE 2:Applicable to 16936 FC method: • Aft upper Trunnion (SSI 57-26-95) aircraft Post-Mod. SB 145-00-0032, under ANAC/FAA Certifications. Applicable to aircraft Post-Mod. SB 145-00Externally inspect the WING components using Eddy Current Inspection 30000 0032, under ANAC/FAA Certifications. Method: • Fwd upper Trunnion (SSI 57-26-96) Applicable to aircraft Post-Mod. SB 145-00Externally inspect the WING components using Eddy Current Inspection 26000 0032, under ANAC/FAA Certifications. Method: • Fwd upper Trunnion (SSI 57-26-96) Externally inspect the WING components using Eddy Current inspection method: • Aft upper Trunnion (SSI 57-26-95) NOTE: Applicable only to trunnion P/N 145-67014-001/002/003/004/005/006/007/008.

20000 FC 21620 FC

EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

17800

16459 FC

EMB-145EP; EMB-145ER; EMB-145EU

11000

10413 FC

EMB-145EP; EMB-145ER; EMB-145EU

22000

20000 FC

EMB-145EP; EMB-145ER; EMB-145EU

30000

20000 FC

EMB-145EP; EMB-145ER; EMB-145EU

-

10000 FC

ALL

Externally inspect the WING components: • Ribs, torque box (SSI 57-2860)

-

7229 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

Externally inspect the WING components: • Lower skin, torque box (SSI 57-28-58)

-

5000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

GVI

-

Externally inspect the WING components: • Spar 3 Attachment, torque box (SSI 57-28-63)

-

10000 FC

ALL

STRUCTURAL

GVI

-

Internally inspect the WING components: • Lower skin, torque box (SSI 57-28-58)

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-28-00-210-807-A00

STRUCTURAL

GVI

-

Internally inspect the WING components: • Spar 3 attachment, torque box 2 (SSI 57-28-63)

-

10000 FC

ALL

57-28-00-210-808-A00

STRUCTURAL

GVI

-

Externally inspect the WING components: • Attachment center flap outboard track (SSI 57-28-68)

-

3912 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-28-00-210-813-A00

STRUCTURAL

GVI

-

Internally inspect the WING components: • Ribs, torque box (SSI 57-2860)

-

10000 FC

ALL

Externally inspect the WING components using Eddy Current Inspection Method: • Aft upper Trunnion (SSI 57-26-95) NOTE: Applicable only to trunnion P/N 145-67014-011/012. Externally inspect the WING components using Eddy Current Inspection Method: • Aft upper Trunnion (SSI 57-26-95) NOTE: Applicable only to trunnion P/N 145-67014-009/010/013/014. Externally inspect the WING components using Eddy Current Inspection Method: • Fwd upper Trunnion (SSI 57-26-96) Internally inspect the WING components: • Spar attachment, torque box (SSI 57-28-57)

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-24 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

57-28-00-210-815-A00

STRUCTURAL

GVI

-

57-28-00-220-801-A00

STRUCTURAL

DET

-

57-28-00-220-805-A00

STRUCTURAL

DET

-

57-28-00-220-806-A00

STRUCTURAL

DET

-

57-28-00-220-807-A00

STRUCTURAL

DET

-

Externally inspect the WING components: • Center track and rib15 trailing edge (SSI 57-28-69)

57-28-00-220-807-A01

STRUCTURAL

DET

-

Externally inspect the WING components: • Center track and rib15 trailing Applicable to A/C Post-Mod SB 145-57-0008 edge (SSI 57-28-69) (Applicable to all A/C Aerolitoral ERJ145fleet)

57-28-00-220-813-A00

STRUCTURAL

DET

-

57-28-00-250-803-A00

STRUCTURAL

SDE

-

57-28-00-250-804-A00

STRUCTURAL

SDE

-

57-28-00-250-805-A00

STRUCTURAL

SDE

-

57-28-00-250-806-A00

STRUCTURAL

SDE

-

57-28-00-250-807-A00

STRUCTURAL

SDE

-

57-29-00-210-801-A00

STRUCTURAL

GVI

-

57-29-00-210-802-A00

STRUCTURAL

GVI

-

57-29-00-210-803-A00

STRUCTURAL

GVI

-

57-41-00-220-801-A00

STRUCTURAL

DET

-

57-42-00-220-801-A00

STRUCTURAL

DET

-

57-43-00-220-801-A00

STRUCTURAL

DET

-

57-50-00-220-801-A00

STRUCTURAL

DET

-

57-50-00-220-802-A00

STRUCTURAL

DET

-

57-50-00-220-803-A00

STRUCTURAL

DET

-

57-50-00-220-804-A00

STRUCTURAL

DET

-

Descripción / Description

Externally inspect the WING components: • Upper skin torque box (SSI 57-28-61) Externally inspect the WING components: • Tracks/ribs attachment, torque box (SSI 57-28-62) Externally inspect the WING components: • Ribs, torque box 3 (SSI 57-2864) Internally inspect the WING components: • Ribs, torque box 3 (SSI 57-2864)

Internally inspect the WING components: • Spar attachment torque box (SSI 57-28-57) Externally inspect the WING components by the Eddy Current Inspection Method: • Spar attachment, torque box (SSI 57-28-57) Internally inspect the WING components by the Eddy Current Inspection Method: • Spar attachment, torque box (SSI 57-28-57) Externally inspect the WING components by the Eddy Current Inspection Method: • Flap track, torque box (SSI 57-28-59) Externally inspect the WING components by the Eddy Current Inspection Method: • Ribs, torque box (SSI 57-28-60) Internally inspect the WING components by the Eddy Current Inspection Method: • Ribs, torque box (SSI 57-28-60) Internally inspect the WING components: • Ribs, main landing gear bay (SSI 57-29-71) Externally inspect the WING components: • Skin/rib attachment, MLGB (SSI 57-29-72) Internally inspect the WING components: • Skin/rib attachment, MLGB (SSI 57-29-72) Internally inspect the WING LEADING EDGE components: • Machined rib flange (SSI 57-41-98) Internally inspect the WING LEADING EDGE components: • Machined rib flange (SSI 57-42-98) Internally inspect the WING LEADING EDGE components: • Machined rib flange (SSI 57-43-98) Externally inspect the FLAP components: • Fitting, root spar, flaps (SSI 57-50-74) Internally inspect the FLAP components: • Fitting, root spar, flaps (SSI 5750-74) Externally inspect the FLAP components: • Roller attachment, flaps (SSI 57-50-76) Externally inspect the FLAP components: • Flap Rollers and Torque Boxes Rollers (SSI 57-50-78)

Applicable to A/C Pre-Mod SB 145-57-0008 (Not Applicable all Aerolitoral EJ145fleet)

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

5445 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

10000 FC

ALL

-

6306 FC

ALL

-

6306 FC

ALL

-

2000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

3275 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

30000

20000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR

-

30000 FC

ALL

-

30000 FC

ALL

-

22633 FC

ALL

-

15824 FC

ALL

-

15824 FC

ALL

-

5000 FC

ALL

-

2500 FC

ALL

-

5000 FC

ALL

-

10000 FC

ALL

-

10000 FC

ALL

-

10000 FC

ALL

-

10000 FC

ALL

-

10000 FC

ALL

-

5000 FC

ALL

-

10000 FC

ALL F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 4. REQUERIMIENTOS DE INSPECCION ESTRUCTURALES

Fecha de Efectividad: 05-Abr-10 Page: 4 -1-25 .

"STRUCTURE INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

57-50-00-240-801-A00

STRUCTURAL

SDE

-

57-50-00-250-801-A00

STRUCTURAL

SDE

-

57-50-00-250-802-A00

STRUCTURAL

SDE

-

57-52-00-210-802-A00

STRUCTURAL

GVI

-

57-52-00-210-803-A00

STRUCTURAL

GVI

-

57-52-00-210-804-A00

STRUCTURAL

GVI

-

57-52-00-220-802-A00

STRUCTURAL

DET

-

57-52-00-220-803-A00

STRUCTURAL

DET

-

57-53-00-210-802-A00

STRUCTURAL

GVI

-

57-53-00-210-803-A00

STRUCTURAL

GVI

-

57-53-00-210-804-A00

STRUCTURAL

GVI

-

57-53-00-210-805-A00

STRUCTURAL

GVI

-

57-53-00-220-801-A00

STRUCTURAL

DET

-

57-53-00-220-802-A00

STRUCTURAL

DET

-

57-53-00-220-805-A00

STRUCTURAL

DET

-

57-61-00-220-801-A00

STRUCTURAL

DET

-

57-61-00-220-802-A00

STRUCTURAL

DET

-

Descripción / Description Externally inspect the FLAP components by the magnetic particle inspection method: • Flap rollers and Torque boxes rollers (SSI 57-50-78) Externally inspect the FLAP components by the Eddy Current Inspection Method: • Roller attachment (SSI 57-50-76) Externally inspect the FLAP components by the Eddy Current Inspection Method: • Tracks, flaps (SSI 57-50-80) Internally inspect the FLAP components: • Ribs/skin attachment, inboard flap (SSI 57-52-79) Externally inspect the FLAP components: • Ribs/skin attachment, inboard flap (SSI 57-52-79) Externally inspect the FLAP components: • Vane inboard/outboard fittings, inboard flap (SSI 57-52-81) Internally inspect the FLAP components: • Fitting tip, inboard flap (SSI 5752-73) Externally inspect the FLAP components: • Vane center fitting, inboard flap (SSI 57-52-78) Internally inspect the FLAP components: • Ribs/skin attachment, outboard flap (SSI 57-53-86) Externally inspect the FLAP components: • Ribs/skin attachment, outboard flap (SSI 57-53-86) Externally inspect the FLAP components: • Vane inboard/outboard fittings, outboard flap (SSI 57-53-88) Internally inspect the FLAP components: • Center ribs attachment, outboard flap (SSI 57-53-87) Externally inspect the FLAP components: • Fitting, tip spar, outboard flap (SSI 57-53-83) Internally inspect the FLAP components: • Fitting, tip spar, outboard flap (SSI 57-53-83) Internally inspect the FLAP components: • Vane center fitting outboard flap (SSI 57-53-85) Externally inspect the AILERON components: • Actuator attachment, aileron (SSI 57-61-90) Internally inspect the AILERON components: • Actuator attachment, aileron (SSI 57-61-90)

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

30000 FC

ALL

-

30000 FC

ALL

-

22633 FC

ALL

-

10000 FC

ALL

-

2500 FC

ALL

-

2500 FC

ALL

-

16797 FC

ALL

-

3447 FC

ALL

-

10000 FC

ALL

-

2500 FC

ALL

-

2500 FC

ALL

-

20000 FC

ALL

-

10000 FC

ALL

-

16797 FC

ALL

-

3447 FC

ALL

-

5000 FC

ALL

-

10000 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-145XR

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 5. PROGRAMA DE PREVENCION Y CONTROL DE LA CORROSION

Fecha de Efectividad: 05-Abr-10 Page: 5 -1- 1 .

"CORROSION PREVENTION & CONTROL PROGRAM CPCP"

Número de Tarea Task Number 32-10-00-210-C01-A00 32-10-00-210-C02-A00 32-10-00-210-C03-A00 32-10-00-210-C04-A00 32-10-00-210-C05-A00 32-10-00-210-C06-A00 32-20-00-210-C01-A00

Grupo Group CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

Tipo Type

Cat. Cat.

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

60 MOS

ALL

-

30 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

-

30 MOS

ALL

-

30 MOS

ALL

-

120 MOS

ALL

-

30 MOS

ALL

-

60 MOS

ALL

Only aircraft equipped with SIDE HINGED MAIN DOR model.

-

120 MOS

ALL

Only aircraft equipped with SIDE HINGED MAIN DOR model.

96 MOS

60 MOS

ALL

Only aircraft equipped with STANDARD MAIN DOOR model.

48 MOS

30 MOS

ALL

Only aircraft equipped with SIDE HINGED MAIN DOR model.

48 MOS

30 MOS

ALL

48 MOS

30 MOS

ALL

-

120 MOS

ALL

72 MOS

30 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

-

120 MOS

ALL

120 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

Descripción / Description Externally inspect the MAIN LANDING GEAR components: • Leg structure, equipped (left) -MLG (SSI 32-10-01) Externally inspect the MAIN LANDING GEAR components: • Shock absorber piston tube assy - MLG (SSI 32-10-05) Externally inspect the MAIN LANDING GEAR components: • Leg structure, equipped (right) -MLG (SSI 32-10-02) Externally inspect the MAIN LANDING GEAR components: • Upper secondary side strut assy - MLG (SSI 32-10-09) Externally inspect the MAIN LANDING GEAR components: • Lower secondary side strut assy - MLG (SSI 32-10-10) Externally inspect the MAIN LANDING GEAR components: • Shock absorber cylinder assy - MLG (SSI 32-10-06) Externally inspect the NOSE LANDING GEAR components: • Main drag strut botton stay -NLG (SSI 32-20-14)

52-10-00-220-C01-A01

CORROSION PROGRAM

DET

CPCP

Internally inspect the MAIN DOOR (SIDE-HINGED MODEL) components: • Attachment fittings-to-fuselage & interface parts (SSI 52-10-05)

52-10-00-220-C02-A00

CORROSION PROGRAM

DET

CPCP

Externally inspect the MAIN DOOR (STANDARD MODEL) components: • Only aircraft equipped with STANDARD MAIN Attachment fittings-to-fuselage & interface parts (SSI 52-10-05) DOOR model.

52-10-00-220-C02-A01

CORROSION PROGRAM

DET

CPCP

Externally inspect the MAIN DOOR (SIDE-HINGED MODEL) components: • Attachment fittings-to-fuselage & interface parts (SSI 5210-05)

52-10-00-220-C04-A01

CORROSION PROGRAM

DET

CPCP

Internally inspect the MAIN DOOR components: • Window frame (SSI 5210-06)

52-10-00-220-C05-A01

CORROSION PROGRAM

DET

CPCP

Externally inspect the MAIN DOOR components: • Window frame (SSI 5210-06)

52-10-00-220-C06-A00

CORROSION PROGRAM

DET

CPCP

Externally inspect the MAIN DOOR (STANDARD MODEL) components: • Structure (SSI 52-10-01)

52-10-00-220-C06-A01

CORROSION PROGRAM

DET

CPCP

Externally inspect the MAIN DOOR (SIDE-HINGED MODEL) components: • Structure (SSI 52-10-01)

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

DET

CPCP

DET

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

52-30-00-210-C01-A00 52-30-00-210-C02-A00 52-43-00-210-C01-A00 52-43-00-210-C02-A00 52-43-00-220-C01-A00 52-43-00-220-C02-A00 53-11-00-210-C01-A00 53-11-00-210-C02-A00 53-11-00-210-C03-A00

CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

Externally inspect the BAGGAGE DOOR components: • Baggage door structure (SSI 52-30-08) Internally inspect the BAGGAGE DOOR components: • Baggage door structure (SSI 52-30-08) Externally inspect the SERVICE DOOR components: • Service door structure (SSI 52-43-10) Internally inspect the SERVICE DOOR components: • Service door structure (SSI 52-43-10) Externally inspect the SERVICE DOOR components: • Service door-tofuselage attachment fittings & interface parts (SSI 52-43-15) Internally inspect the SERVICE DOOR components: • Service door-tofuselage attachment fittings & interface parts (SSI 52-43-15) Internally inspect the FUSELAGE components: Bulkhead 1 structure (SSI 53-10-23) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-10-07) Externally inspect the FUSELAGE components: • Nose landing gear bay structure (SSI 53-10-24)

Only aircraft equipped with SIDE HINGED MAIN DOR model.

Only aircraft equipped with SIDE HINGED MAIN DOR model.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 5. PROGRAMA DE PREVENCION Y CONTROL DE LA CORROSION

Fecha de Efectividad: 05-Abr-10 Page: 5 -1- 2 .

"CORROSION PREVENTION & CONTROL PROGRAM CPCP"

Número de Tarea Task Number 53-11-00-210-C05-A00 53-11-00-210-C06-A00 53-11-00-210-C07-A00 53-11-00-210-C08-A00 53-11-00-220-C01-A00 53-11-00-220-C01-A01 53-11-00-220-C02-A00 53-11-00-220-C03-A00 53-11-00-220-C04-A00 53-11-00-220-C05-A00 53-11-00-220-C07-A00 53-12-00-210-C01-A00 53-12-00-210-C03-A00 53-12-00-210-C04-A00 53-12-00-210-C05-A00 53-12-00-210-C07-A00 53-12-00-210-C10-A00 53-12-00-210-C11-A00 53-12-00-210-C12-A00 53-12-00-220-C01-A00 53-12-00-220-C02-A00 53-12-00-220-C03-A00 53-12-00-220-C04-A00 53-12-00-220-C06-A00 53-12-00-220-C07-A00 53-12-00-220-C08-A00

Grupo Group CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

Tipo Type

Cat. Cat.

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

Descripción / Description Internally inspect the FUSELAGE components: • Nose landing gear bay structure (SSI 53-10-24) Internally inspect the FUSELAGE components: • Battery compartment cutout structure (SSI 53-10-44) Internally inspect the FUSELAGE components: • Hydraulic compartment cutout structure (SSI 53-10-45) Internally inspect the FUSELAGE components: • Longerons (SSI 53-1046) Internally inspect the FUSELAGE components: • Nose landing gear fitting, including bearing cap and trunnion fitting (SSI 53-10-25) Internally inspect the FUSELAGE components: • Nose landing gear fitting, including bearing cap and trunnion fitting (SSI 53-10-25) Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-10-07) Internally inspect the FUSELAGE components: • Fuselage skin Circumferential splice (SSI 53-10-14) Internally inspect the FUSELAGE components: • Fuselage skin panel at pressure bulkhead SSI 53-10-15)

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP Internally inspect the FUSELAGE components: • Frames (SSI 53-10-43) Externally inspect the FUSELAGE components: • Fuselage skin panel at pressure bulkhead (SSI 53-10-15) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-10-07) Externally inspect the FUSELAGE components: • Windshield cutout structure (SSI 53-10-17) Externally inspect the FUSELAGE components: • Windshield center post, including its attachments and lower fitting (SSI 53-10-19) Externally inspect the FUSELAGE components: • Maintenance door cutout structure (SSI 53-10-49) Internally inspect the FUSELAGE components: • Windshield panel (SSI 53-10-21) Externally inspect the FUSELAGE components: • Cockpit window cutout structure (SSI 53-10-18) Externally inspect the FUSELAGE components: • Windshield panel (SSI 53-10-21) Externally inspect the FUSELAGE components: • Cockpit window rear post and its attachment (SSI 53-10-22) Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-10-07) Internally inspect the FUSELAGE components: • Fuselage skin longitudinal splice (SSI 53-10-08) Internally inspect the FUSELAGE components: • Fuselage skin circumferential splice (SSI 53-10-14) Internally inspect the FUSELAGE components: • Cockpit floor beams and columns (SSI 53-10-27) Internally inspect the FUSELAGE components: • Fuselage skin panel at pressure bulkhead (SSI 53-10-15)

DET

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP Internally inspect the FUSELAGE components: • Frames (SSI 53-10-43)

DET

CPCP

Internally inspect the FUSELAGE components: • Maintenance door cutout structure (SSI 53-10-49)

Applicable to aircraft Pre-Mod. SB 145-320063. Applicable to aircraft Post-Mod. SB 145-320063.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

96 MOS

60 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

-

15 MOS

ALL

-

30 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

-

120 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 5. PROGRAMA DE PREVENCION Y CONTROL DE LA CORROSION

Fecha de Efectividad: 05-Abr-10 Page: 5 -1- 3 .

"CORROSION PREVENTION & CONTROL PROGRAM CPCP"

Número de Tarea Task Number 53-12-00-220-C09-A00 53-21-00-210-C02-A00 53-21-00-210-C03-A00 53-21-00-220-C03-A00 53-21-00-220-C05-A00 53-21-00-220-C06-A00

Grupo Group CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

Tipo Type

Cat. Cat.

DET

CPCP

GVI

CPCP

GVI

CPCP

DET

CPCP

DET

CPCP

DET

CPCP Internally inspect the FUSELAGE components: • Frames (SSI 53-20-43)

Descripción / Description Externally inspect the FUSELAGE components: • Fuselage Skin Panel at pressure bulkhead (SSI 53-10-15) Externally inspect the FUSELAGE components: • Main door attachments fittings and interface parts (SSI 53-20-04) Externally inspect the FUSELAGE components: • Service door attachment fittings and interface parts (SSI 53-20-05) Internally inspect the FUSELAGE components: • Stops and backup structures for service door (SSI 53-20-02) Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07)

53-21-00-220-C07-A00

CORROSION PROGRAM

DET

CPCP

Internally inspect the FUSELAGE components: • Passenger cabin floor beams and columns (SSI 53-20-11)

53-21-00-220-C07-A01

CORROSION PROGRAM

DET

CPCP

Internally inspect the FUSELAGE components: • Passenger cabin floor beams and columns (SSI 53-20-11) NOTE: Applicable to aircraft PostMod. SB 145-53- 0026, SB 145-53-0039 and SB 145-53-0041

53-22-00-210-C03-A00 53-22-00-220-C01-A00 53-22-00-220-C02-A00 53-22-00-220-C02-A01 53-22-00-220-C03-A00 53-22-00-220-C04-A00 53-22-00-220-C05-A00 53-22-00-220-C06-A00

CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

GVI

CPCP

DET

CPCP

DET

CPCP

CORROSION PROGRAM

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP Internally inspect the FUSELAGE components: • Frames (SSI 53-20-43)

CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

NOTE: Applicable to aircraft Pre-Mod. SB 14553-0026 or SB 145-53-0039 or SB 145-530041.

Externally inspect the FUSELAGE components: • Passenger cabin window frame (SSI 53-20-06) Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07) Internally inspect the FUSELAGE components: • Passenger cabin floor NOTE: Applicable to aircraft Pre-Mod. SB 14553-0041. beams and columns (SSI 53-20-11) Internally inspect the FUSELAGE components: • Passenger cabin floor beams and columns (SSI 53-20-11) NOTE: Applicable to aircraft PostMod. SB 145-53-0041. Internally inspect the FUSELAGE components: • Passenger cabin window frame (SSI 53-20-06) Internally inspect the FUSELAGE components: • Fuselage skin longitudinal splice(SSI 53-20-08) Internally inspect the FUSELAGE components: • Fuselage skin circumferential splice (SSI 53-20-14)

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

96 MOS

60 MOS

ALL

72 MOS

30 MOS

ALL

72 MOS

30 MOS

ALL

-

30 MOS

ALL

-

30 MOS

ALL

-

60 MOS

ALL

-

24 MOS

ALL

-

30 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

-

48 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

53-23-00-210-C01-A00

CORROSION PROGRAM

GVI

CPCP

Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07)

-

60 MOS

EMB-145EU EMB-145EP EMB-145ER EMB-145XR EMB-135ER EMB-135LR EMB-135KE EMB-135KL

53-23-00-210-C02-A00

CORROSION PROGRAM

GVI

CPCP

Externally inspect the FUSELAGE components: • Passenger cabin window frame (SSI 53-20-06)

-

60 MOS

EMB-145EU EMB-145EP EMB-145ER EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-135ER EMB-135LR EMB-135KE EMB-135KL

-

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

53-23-00-210-C04-A00 53-23-00-220-C01-A00 53-23-00-220-C02-A00 53-23-00-220-C03-A00

CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

GVI DET DET DET

Internally inspect the FUSELAGE components: • Passenger cabin window frame (SSI 53-20-06) Internally inspect the FUSELAGE components: • Fuselage skin panel at CPCP stringers, frames/bulkheads, and splices (SSI 53-20-07) CPCP

CPCP Internally inspect the FUSELAGE components: • Frames (SSI 53-20-43) CPCP

Internally inspect the FUSELAGE components: • Fuselage skin longitudinal splice (SSI 53-20-08)

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 5. PROGRAMA DE PREVENCION Y CONTROL DE LA CORROSION

Fecha de Efectividad: 05-Abr-10 Page: 5 -1- 4 .

"CORROSION PREVENTION & CONTROL PROGRAM CPCP"

Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

53-23-00-220-C04-A00

CORROSION PROGRAM

DET

CPCP

53-23-00-220-C04-A01

CORROSION PROGRAM

DET

CPCP

DET

CPCP

DET

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

53-23-00-220-C05-A00 53-23-00-220-C06-A00 53-24-00-210-C01-A00 53-24-00-210-C02-A00 53-24-00-210-C03-A00

CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

53-24-00-210-C04-A00

CORROSION PROGRAM

53-24-00-210-C08-A00

CORROSION PROGRAM

53-24-00-220-C01-A00 53-24-00-220-C02-A00

CORROSION PROGRAM CORROSION PROGRAM

GVI

GVI

DET DET

Descripción / Description Internally inspect the FUSELAGE components: • Passenger cabin floor NOTE: Applicable to aircraft Pre-Mod. SB 14553-0041. beams and columns (SSI 53-20-11) Internally inspect the FUSELAGE components: • Passenger cabin floor beams and columns (SSI 53-20-11) NOTE: Applicable to aircraft PostMod. SB 145-53-0041. Internally inspect the FUSELAGE components: • Skin and reinforcement around escape hatch cutout (SSI 53-20-51) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07) Internally inspect the FUSELAGE components: • Passenger cabin window frame (SSI 53-20-06) Externally inspect the FUSELAGE components: • Passenger cabin window frame (SSI 53-20-06)

CPCP

Internally inspect the FUSELAGE components: • Fuselage skin circumferential splice (SSI 53-20-14)

CPCP

Externally inspect the FUSELAGE components: • Toilets waste valve support (SSI 53-20-29)

Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-20-07) Internally inspect the FUSELAGE components: • Passenger cabin floor NOTE: Applicable to aircraft Pre-Mod. SB 145CPCP 53-0026 or SB 145-53-0041. beams and Columns (SSI 53-20-11) Internally inspect the FUSELAGE components: • Passenger cabin floor CPCP beams and columns (SSI 53-20-11) NOTE: Applicable to aircraft PostMod. SB 145-53-0026 and SB 145-53-0041. CPCP

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

48 MOS

ALL

-

60 MOS

ALL

96 MOS

60 MOS

ALL

-

60 MO

ALL

-

30 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

60 MOS

EMB-145EU EMB-145EP EMB-145ER EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-135ER EMB-135LR EMB-135KE EMB-135KL

-

30 MOS

EMB-145EP EMB-145ER EMB-145EU EMB-145LR EMB-145LU EMB-145MK EMB-145MP EMB-145MR EMB-145XR EMB-135ER EMB-135LR EMB-135KE EMB-135KL

-

60 MOS

ALL

-

48 MOS

ALL

-

60 MOS

ALL EMB-145LR EMB-145LU EMB-145MK EMB-145MP EMB-145MR EMB-135ER EMB-135LR EMB-135KE EMB-135KL

-

53-24-00-220-C02-A01

CORROSION PROGRAM

DET

53-24-00-220-C03-A00

CORROSION PROGRAM

DET

CPCP

Internally inspect the FUSELAGE components: • Fuselage skin longitudinal splice (SSI 53-20-08)

-

60 MOS

53-24-00-220-C04-A00

CORROSION PROGRAM

DET

CPCP

Internally inspect the FUSELAGE components:• Frames (SSI 53-20-43)

-

60 MOS

ALL

53-24-00-220-C06-A00

53-24-00-220-C07-A00 53-31-00-220-C01-A00 53-31-00-220-C02-A00 53-31-00-220-C03-A00 53-31-00-220-C04-A00

CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

DET

CPCP

Internally inspect the FUSELAGE components: • Toilet waste valve support (SSI 53-20-29)

-

30 MOS

EMB-145EP EMB-145ER EMB-145EU EMB-145LR EMB-145LU EMB-145MK EMB-145MP EMB-145MR EMB-145XR EMB-135ER EMB-135LR EMB-135KE EMB-135KL

DET

CPCP

Internally inspect the FUSELAGE components: • fuselage skin longitudinal splice(SSI 53-20-08)

-

60 MOS

EMB-145EP EMB-145ER EMB-145EU

DET

CPCP

Internally inspect the FUSELAGE components: •Frames(SSI 53-30-43)

-

30 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

-

30 MOS

ALL

DET DET DET

Internally inspect the FUSELAGE components: • Fuselage skin panel at CPCP stringers, frames/bulkheads, and splices (SSI 53-30-07) Internally inspect the FUSELAGE components: • Fuselage skin panel at CPCP pressure bulkhead (SSI 53-30-15) Internally inspect the FUSELAGE components: • Fuselage skin CPCP circumferential splice (SSI 53-30-14)

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 5. PROGRAMA DE PREVENCION Y CONTROL DE LA CORROSION

Fecha de Efectividad: 05-Abr-10 Page: 5 -1- 5 .

"CORROSION PREVENTION & CONTROL PROGRAM CPCP"

Número de Tarea Task Number 53-31-00-220-C05-A00 53-31-00-220-C07-A00 53-31-00-220-C08-A00

Grupo Group CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

Tipo Type

Cat. Cat.

DET

CPCP

DET DET

Descripción / Description

Internally inspect the FUSELAGE components: • Fuselage skin panel at pressure bulkhead (SSI 53-30-15) Internally inspect the FUSELAGE components: • Rear pressure bulkhead CPCP (SSI 53-30-36) CPCP

Internally inspect the FUSELAGE components:• Frames (SSI 53-30-43)

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

30 MOS

ALL

-

30 MOS

ALL

-

30 MOS

ALL

53-31-00-220-C09-A00

CORROSION PROGRAM

DET

CPCP

Internally inspect the FUSELAGE components: • Fuselage skin longitudinal splice (SSI 53-30-08)

96 MOS

60 MOS

EMB-145LR EMB-145LU EMB-145MK EMB-145MP EMB-145MR EMB-145XR EMB-135ER EMB-135LR EMB-135KE EMB-135KL

53-31-00-220-C10-A00

CORROSION PROGRAM

DET

CPCP

Internally inspect the FUSELAGE components: • Rear pressure bulkhead (SSI 53-30-36)

-

60 MOS

ALL

53-31-00-220-C11-A00

CORROSION PROGRAM

DET

CPCP

Internally inspect the FUSELAGE components: •Fuselage skin longitudinal splice (SSI 53-30-08)

96 MOS

60 MOS

EMB-145EP EMB-145ER EMB-145EU

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

48 MOS

30 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

-

30 MOS

ALL

-

30 MO

ALL

-

30 MO

ALL

-

60 MOS

ALL

-

15 MOS

ALL

96 MOS

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

53-32-00-210-C01-A00 53-32-00-210-C02-A00 53-32-00-210-C05-A00 53-32-00-220-C01-A00 53-32-00-220-C02-A00 53-32-00-220-C03-A00 53-32-00-220-C04-A00 54-50-00-220-C01-A00 54-50-00-220-C02-A00 54-50-00-220-C03-A00 55-10-00-210-C02-A00 55-10-00-210-C03-A00 55-10-00-210-C05-A00

CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

GVI GVI GVI DET DET

Externally inspect the FUSELAGE component: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-30-07) Internally inspect the FUSELAGE components: • Fuselage skin panel at CPCP stringers, frames/bulkheads, and splices (SSI 53-30-07) Internally inspect the FUSELAGE components: • Tail cone frame at APU CPCP mounting attachment (SSI 53-30-39) Internally inspect the FUSELAGE components: • Rear pressure bulkhead CPCP (SSI 53-30-36) CPCP

CPCP Internally inspect the FUSELAGE components: • Frames (SSI 53-30-43)

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

GVI

CPCP

GVI

CPCP

GVI

Internally inspect the FUSELAGE components: • Fuselage skin longitudinal splice (SSI 53-30-08) Internally inspect the FUSELAGE components: • Fuselage skin circumferential splice (SSI 53-30-14) Internally inspect the PYLON components: • Pylon yokes III and IV (SSI 54-50-02) Internally inspect the PYLON components: • Pylon yokes I and II (SSI 5450-05) Internally inspect the PYLON components: Pylon yokes I and II upper flange (SSI 54-50-06) Externally inspect the HORIZONTAL STABILIZER components: • U shape, L shape and box structure - elevator command (SSI 55-10-22)

Externally inspect the HORIZONTAL STABILIZER components: • Pin, internal and external hinge, stabilizer (SSI 55-10-24) Externally inspect the HORIZONTAL STABILIZER components: • Support CPCP quadrant assy, stabilizer (SSI 55-10-23)

55-10-00-210-C06-A00

CORROSION PROGRAM

GVI

CPCP

55-10-00-220-C01-A00

CORROSION PROGRAM

DET

CPCP

55-10-00-220-C02-A00

CORROSION PROGRAM

DET

55-10-00-220-C03-A00

CORROSION PROGRAM

DET

Externally inspect the HORIZONTAL STABILIZER components: • Skin, from rib sta. YH= 990 to rib sta. YH=2965- lower surface (SSI 55-10-08)

Internally inspect the HORIZONTAL STABILIZER components: • Ribs, from rib sta. YH= 990 to rib sta. YH=2965 (SSI 55-10-05) Externally inspect the HORIZONTAL STABILIZER components: • Skin, CPCP from rib sta. YH= 990 to rib sta. YH=2965- upper surface (SSI 55-10-03) Internally inspect the HORIZONTAL STABILIZER components: • Front spar web and cap, from rib sta. YH= 350 to rib sta. CPCP YH=2965 (SSI 55-10-10) Internally inspect the HORIZONTAL STABILIZER

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 5. PROGRAMA DE PREVENCION Y CONTROL DE LA CORROSION

Fecha de Efectividad: 05-Abr-10 Page: 5 -1- 6 .

"CORROSION PREVENTION & CONTROL PROGRAM CPCP"

Número de Tarea Task Number

Grupo Group

Tipo Type

55-10-00-220-C04-A00

CORROSION PROGRAM

DET

55-10-00-220-C05-A00

CORROSION PROGRAM

DET

55-10-00-220-C06-A00 55-20-00-210-C01-A00 55-20-00-210-C02-A00 55-20-00-210-C03-A00 55-20-00-210-C04-A00 55-20-00-210-C05-A00 55-20-00-220-C02-A00 55-20-00-220-C03-A00 55-20-00-220-C05-A00 55-20-00-220-C06-A00 55-20-00-290-C01-A00 55-20-00-290-C02-A00

CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

DET GVI GVI GVI GVI

Cat. Cat.

Descripción / Description

components: • Front spar web and cap, from fin to rib sta. YH= 350, CPCP including center fitting/spar attachment (SSI 55-10-09) Internally inspect the HORIZONTAL STABILIZER components• Rear spar web & cap, from rib sta. YH= 350 to rib sta. CPCP YH=2965, including fitting hinge stabilizer attach to elevator (SSI 55-1013) Internally inspect the HORIZONTAL STABILIZER components: • Ribs, CPCP from rib sta. YH= 30 to rib sta. YH= 990 (SSI 55-10-04) Externally inspect the ELEVATOR components: • Skin, between root and CPCP sta. YH=160 (SSI 55-20-26) Internally inspect the ELEVATOR components: • Spars between root and CPCP sta. YH=160 (SSI 55-20-25) Externally inspect the ELEVATOR components: • Skin, between sta. CPCP YH=160 and sta. YH= 3320 (SSI 55-20-28) CPCP

GVI

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

SDE

CPCP

SDE

CPCP

55-30-00-210-C01-A00

CORROSION PROGRAM

GVI

CPCP

55-30-00-210-C02-A00

CORROSION PROGRAM

GVI

CPCP

55-30-00-210-C03-A00

CORROSION PROGRAM

GVI

CPCP

55-30-00-210-C04-A00

CORROSION PROGRAM

GVI

CPCP

55-30-00-210-C05-A00

CORROSION PROGRAM

GVI

CPCP

55-30-00-210-C06-A00

CORROSION PROGRAM

GVI

CPCP

55-30-00-210-C07-A00

CORROSION PROGRAM

GVI

CPCP

55-30-00-210-C08-A00

CORROSION PROGRAM

GVI

CPCP

Externally inspect the ELEVATOR components: • Tab (SSI 55-20-37) Internally inspect the ELEVATOR components: • Spars, between sta. YH=160 and sta. YH= 3320 (SSI 55-20-27) Internally inspect the ELEVATOR components: • Ribs, between root and sta. YH=160 (SSI 55-20-29) Externally inspect the ELEVATOR components: • Tab Hinge Fittings (SSI 55-20-36) Internally inspect the ELEVATOR components: • Ribs, between sta. YH=160 and sta. YH= 983.4 (SSI 55-20-30) Internally inspect the ELEVATOR components: • Ribs, between sta. YH= 3001 and sta YH=3320 (SSI 55-20-33) Internally inspect the ELEVATOR components using a boroscope: • Ribs, between sta. YH= 983,4 and sta YH= 1898 (SSI 55-20-31) Internally inspect the ELEVATOR components using a boroscope: • Ribs, between sta. YH= 1898 and sta YH= 3001(SSI 55-20-32) Externally inspect the VERTICAL STABILIZER components: • Skin at spars 1, 2, auxiliary spar 41% and stringers 20% & 35.5% between fuselage & rib sta. ZV=1169 (SSI 55-30-38) Externally inspect the VERTICAL STABILIZER components: • Skin at spar 3, auxiliary spar 52% and stringers 46.5% & 57.65%, between fuselage & rib sta. ZV=1169 (SSI 55-30-39) Externally inspect the VERTICAL STABILIZER components: • Skin at ribs from fuselage to sta. ZV=1169 (SSI 55-30-47) Internally inspect the VERTICAL STABILIZER components: • Ribs (sta. ZV=3461, ZV=2538, ZV=1677, ZV=1550.5, ZV=1430.5, ZV=1423, ZV=1302, ZV=1169 and ZV=915) (SSI 55-30-73) Externally inspect the VERTICAL STABILIZER components: • Skin at spars 1, 2, auxiliary spar 41% and stringers 20% & 35.5% between ribs sta. ZV=1169 & sta. ZV=2799 (SSI 55-30-40) Externally inspect the VERTICAL STABILIZER components: • Skin at spars 1, 2, auxiliary spar 41% and stringers 20% & 35.5% between rib sta. ZV=2799 & horizontal stabilizer (SSI 55-30-42) Externally inspect the VERTICAL STABILIZER components: • Skin at windows from fuselage to sta. ZV=1169 (SSI 55-30-44) Externally inspect the VERTICAL STABILIZER components: • Skin at windows between sta. ZV=2799 and horizontal stabilizer (SSI 55-30-46)

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

-

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

72 MOS

30 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

96 MOS

60 MOS

ALL

72 MOS

30 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 5. PROGRAMA DE PREVENCION Y CONTROL DE LA CORROSION

Fecha de Efectividad: 05-Abr-10 Page: 5 -1- 7 .

"CORROSION PREVENTION & CONTROL PROGRAM CPCP"

Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

55-30-00-210-C09-A00

CORROSION PROGRAM

GVI

CPCP

55-30-00-210-C10-A00

CORROSION PROGRAM

GVI

CPCP

GVI

CPCP

GVI

CPCP

55-30-00-210-C11-A00 55-30-00-210-C12-A00

CORROSION PROGRAM CORROSION PROGRAM

55-30-00-210-C13-A00

CORROSION PROGRAM

GVI

CPCP

55-30-00-220-C01-A00

CORROSION PROGRAM

DET

CPCP

55-30-00-220-C02-A00

CORROSION PROGRAM

DET

CPCP

DET

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

55-30-00-220-C03-A00 55-40-00-210-C01-A00 55-40-00-210-C02-A00 55-40-00-210-C03-A00 55-40-00-210-C04-A00 55-40-00-210-C05-A00 55-40-00-210-C06-A00 55-40-00-210-C07-A00 55-40-00-210-C08-A00 55-40-00-210-C09-A00 55-40-00-220-C03-A00 55-40-00-220-C04-A00 55-40-00-220-C05-A00 55-40-00-220-C06-A00 55-40-00-220-C07-A00 55-40-00-220-C08-A00 55-40-00-220-C09-A00

CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

Descripción / Description Externally inspect the VERTICAL STABILIZER components: • Skin at spar 3, auxiliary spar 52% and stringers 46.5% & 57.65%, between ribs sta. ZV=1169 & sta. ZV=2799 (SSI 55-30-41) Externally inspect the VERTICAL STABILIZER components: • Skin at spar 3, auxiliary spar 52%, and stringers 46.5% & 57.65%, between rib sta. ZV=2799 & horizontal stabilizer (SSI 55-30-43) Externally inspect the VERTICAL STABILIZER components: • Skin at windows between sta. ZV=1169 & sta. ZV=2799 (SSI 55-30-45) Externally inspect the VERTICAL STABILIZER components: • Skin at ribs, between sta. ZV=1169 and sta. ZV=2799 (SSI 55-30-48) Externally inspect the VERTICAL STABILIZER components: • Skin at ribs, between sta. ZV=2799 and horizontal stabilizer (SSI 55-30-49) Internally inspect the VERTICAL STABILIZER components: • Root rib, including bolts (SSI 55-30-70) Internally inspect the VERTICAL STABILIZER components: • Ribs of horizontal stabilizer actuators (sta. ZV=3145, ZV=3015 and ZV=2799) (SSI 55-30-71) Internally inspect the VERTICAL STABILIZER components:• Ribs of actuator area (sta. ZV=1932 and ZV=2277) (SSI 55-30-72) Externally inspect the RUDDER components: • Front spar - skin attachment (rudder I) (SSI 55-40-81) Externally inspect the RUDDER components: • Spar - skin attachment (rudder II) (SSI 55-40-86) Externally inspect the RUDDER components: • Rear spar - skin attachment (rudder I) (SSI 55-40-82) Externally inspect the RUDDER components:• LT & RT skin -spar cap attachment (rudder I) (SSI 55-40-83) Externally inspect the RUDDER components: • Ribs - skin attachment (rudder I) (SSI 55-40-84) Externally inspect the RUDDER components: • Hinges - rudder I (SSI 5540-85) Externally inspect the RUDDER components: • LT & RT skin -spar cap attachment (rudderII) (SSI 55-40-87) Externally inspect the RUDDER components:• Ribs - skin attachment (rudder II) (SSI 55-40-88) Externally inspect the RUDDER components: • Hinges - rudder II (SSI 5540-89) Internally inspect the RUDDER components: • Front spar - skin attachment (rudder I) (SSI 55-40-81) Internally inspect the RUDDER components: • Spar - skin attachment (rudder II) (SSI 55-40-86) Internally inspect the RUDDER components: • Rear spar - skin attachment (rudder I) (SSI 55-40-82) Internally inspect the RUDDER components: • LT & RT skin -spar cap attachment (rudder I) (SSI 55-40-83) Internally inspect the RUDDER components: • Ribs - skin attachment (rudder I) (SSI 55-40-84) Internally inspect the RUDDER components: • Hinges - rudder I (SSI 5540-85) Internally inspect the RUDDER components: • LT & RT skin -spar cap attachment (rudder II) (SSI 55-40-87)

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

72 MOS

30 MOS

ALL

72 MOS

30 MOS

ALL

72 MOS

30 MOS

ALL

72 MOS

30 MOS

ALL

72 MOS

30 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 5. PROGRAMA DE PREVENCION Y CONTROL DE LA CORROSION

Fecha de Efectividad: 05-Abr-10 Page: 5 -1- 8 .

"CORROSION PREVENTION & CONTROL PROGRAM CPCP"

Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Descripción / Description

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

-

120 MOS

ALL EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-145XR EMB-135LR EMB-135KE EMB-135KL

CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

DET

57-01-00-220-C02-A00

CORROSION PROGRAM

DET

CPCP

Internally inspect the WING STUB components: • Wing stub - rib 2A skin supports and their attachments to web, lower flange, and FWD & AFT web supports (SSI 57-01-18)

-

60 MOS

57-01-00-220-C03-A00

CORROSION PROGRAM

DET

CPCP

Externally inspect the WING STUB components: • Wing stub - lower skin rib 2A attachment (SSI 57-01-15)

-

120 MOS

57-01-00-220-C04-A00

CORROSION PROGRAM

DET

CPCP

Externally inspect the WING STUB components: • Wing stub - upper skin rib 2A attachment (SSI 57-01-19)

-

60 MOS

57-01-00-220-C05-A00

CORROSION PROGRAM

DET

CPCP

Internally inspect the WING STUB components: • Wing stub - Spar 2 brackets ribs 2A attachments (SSI 57-01-17)

-

120 MOS

57-01-00-220-C06-A00

CORROSION PROGRAM

DET

CPCP

Internally inspect the WING STUB components: • Wing stub - spar 1 brackets ribs 2A attachments (SSI 57-01-16)

-

120 MOS

ALL

-

60 MOS

EMB-145LR EMB-145LU EMB145MR EMB-145MP EMB-145XR EMB145MK EMB-135LR EMB-135KE EMB135KL

-

120 MOS

ALL

-

60 MOS

EMB-145EU EMB-145EP EMB-145ER EMB-135ER

-

30 MOS

ALL

-

60 MOS

ALL

-

120 MOS

EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-145XR EMB-135LR EMB-135KE EMB-135KL

-

30 MOS

55-40-00-220-C10-A00 55-40-00-220-C11-A00 57-01-00-220-C01-A00

57-01-00-220-C07-A00

57-10-00-210-C01-A00 57-10-00-220-C01-A00 57-10-00-220-C02-A00 57-10-00-220-C03-A00

57-10-00-220-C04-A00

57-10-00-220-C05-A00 57-10-00-220-C06-A00 57-10-00-220-C07-A00 57-10-00-220-C08-A00 57-10-00-220-C09-A00 57-10-00-220-C10-A00

CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

DET

DET

DET

GVI DET DET DET

Internally inspect the RUDDER components: • Ribs - skin attachment (rudder II) (SSI 55-40-88) Internally inspect the RUDDER components: • Hinges - rudder II (SSI 55CPCP 40-89) Internally inspect the WING STUB components: • Wing stub - lower skin CPCP rib 2A attachment (SSI 57-01-15) CPCP

CPCP

Internally inspect the WING STUB components: • Wing stub - upper skin rib 2A attachments (SSI 57-01-19)

Externally inspect the WING STUB components: • Upper skin - tire compartment composite panel (SSI 57-10-14) Externally inspect the WING STUB components: • Spar 3 -lower skin CPCP attachments (SSI 57-10-09) Internally inspect the WING STUB components: • Spar 3 -lower skin CPCP attachments (SSI 57-10-09) Internally inspect the WING STUB components: • Spar 1 -brackets, ribs 1 CPCP and 3 attachments (SSI 57-10-04) CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

Internally inspect the WING STUB components: • Upper skin - rib 1 attachments and spanwise splice of integral panel (SSI 57-10-13) Externally inspect the WING STUB components: • Upper skin - rib 1 attachments and spainwise splice of integral panel (SSI 57-10-13) Internally inspect the WING STUB components: • Spar 3 -lower skin attachments (SSI 57-10-09) Internally inspect the WING STUB components: • Spar 3 -center bracket and rib 2 attachments (SSI 57-10-10) Internally inspect the WING STUB components: • Upper skin - rib 1 attachments and spanwise splice of integral panel (SSI 57-10-13) Externally inspect the WING STUB components: • Rib 4 -lower flange and web (SSI 57-10-11) Internally inspect the WING STUB components: • Spar 3 -center bracket and rib 2 attachments (SSI 57-10-10)

EMB-145LR EMB-145LU EMB145MR EMB-145MP EMB-145MK EMB145XR EMB-135LR EMB-135KE EMB135KL EMB-145LR EMB-145LU EMB145MR EMB-145MP EMB-145MK EMB145XR EMB-135LR EMB-135KE EMB135KL EMB-145LR EMB-145LU EMB145MR EMB-145MP EMB-145MK EMB145XR EMB-135LR EMB-135KE EMB135KL

ALL EMB-145EU EMB-145EP EMB-145ER EMB-135ER EMB-145EU EMB-145EP EMB-145ER EMB-135ER EMB-145EU EMB-145EP EMB-145ER EMB-135ER

-

15 MOS

-

60 MOS

-

30 MOS

-

60 MOS

ALL

-

30 MOS

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 5. PROGRAMA DE PREVENCION Y CONTROL DE LA CORROSION

Fecha de Efectividad: 05-Abr-10 Page: 5 -1- 9 .

"CORROSION PREVENTION & CONTROL PROGRAM CPCP"

Número de Tarea Task Number 57-10-00-220-C11-A00 57-10-00-220-C12-A00 57-10-00-220-C13-A00

Grupo Group CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

Tipo Type

Cat. Cat.

DET

CPCP

DET DET

Descripción / Description

Internally inspect the WING STUB components: • Rib 4 -lower flange and web (SSI 57-10-11) Internally inspect the WING STUB components: • Rib 2 -Longitudinal CPCP stringer-to-web attachments (SSI 57-10-12) Internally inspect the WING STUB components: • Upper skin - tire CPCP compartment composite panel (SSI 57-10-14)

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

30 MOS

ALL

-

30 MOS

ALL

-

30 MOS

ALL

57-10-00-220-C14-A00

CORROSION PROGRAM

DET

CPCP

Internally inspect the WING STUB components: • Spar 2 -center brackets & rib 2 attachments and ribs 1 & 3 web attachments (SSI 57-10-07)

-

60 MOS

ALL

57-10-00-220-C15-A00

CORROSION PROGRAM

DET

CPCP

Externally inspect the WING STUB components: • Spar 3 -lower skin attachments (SSI 57-10-09)

-

30 MOS

EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-145XR EMB-135LR EMB-135KE EMB-135KL

GVI

CPCP

Externally inspect the WING components: • Upper skin/spar attachment (SSI 57-21-37)

72 MOS

30 MOS

ALL

GVI

CPCP

Externally inspect the WING components: • Skin panels (SSI 57-21-26)

96 MOS

60 MOS

ALL

GVI

CPCP

Externally inspect the WING components: • Lower vent hole (SSI 57-2133)

96 MOS

60 MOS

EMB-145EU EMB-145EP EMB-145ER EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-135ER EMB-135LR EMB-135KE EMB-135KL

GVI

CPCP

96 MOS

60 MOS

ALL

GVI

CPCP

-

60 MOS

ALL

GVI

CPCP

Internally inspect the WING components: • Lower skin panel spanwise joint (SSI 57-21-30)

-

60 MOS

EMB-145EU EMB-145EP EMB-145ER EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-135ER EMB-135LR EMB-135KE EMB-135KL

GVI

CPCP

Internally inspect the WING components: • Upper skin panel spanwise joint (SSI 57-21-31)

-

60 MOS

ALL

GVI

CPCP

Internally inspect the WING components: • Skin panels (SSI 57-21-26)

96 MOS

60 MOS

ALL

GVI

CPCP

Internally inspect the WING components: • Upper skin/spar stub attachment (SSI 57-21-39)

-

60 MOS

ALL

GVI

CPCP

Internally inspect the WING components: • Skin panels (SSI 57-21-26)

-

120 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

-

30 MOS

ALL

-

60 MOS

ALL

57-21-00-210-C01-A00 57-21-00-210-C02-A00

57-21-00-210-C03-A00

57-21-00-210-C05-A00 57-21-00-210-C06-A00

57-21-00-210-C07-A00

57-21-00-210-C08-A00 57-21-00-210-C09-A00 57-21-00-210-C10-A00 57-21-00-210-C11-A00 57-21-00-210-C12-A00 57-21-00-210-C14-A00 57-21-00-210-C15-A00 57-21-00-210-C16-A00 57-21-00-210-C17-A00 57-21-00-210-C18-A00 57-21-00-210-C19-A00

CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

Externally inspect the WING components: • Upper skin/spar attachment (SSI 57-21-37) Externally inspect the WING components: • Lower skin panel chordwise joint (SSI 57-21-29)

Internally inspect the WING components: • Upper skin panel spanwise joint (SSI 57-21-31) Internally inspect the WING components: • Lower vent hole (SSI 57-2133) Internally inspect the WING components: • Lower skin panel span wise joint (SSI 57-21-30) Internally inspect the WING components: • Upper skin/spar attachment (SSI 57-21-37) Internally inspect the WING components: • Lower skin/wing stub attachment (SSI 57-21-38) Externally inspect the WING components: • Upper skin/wing stub attachment (SSI 57-21-39) Externally inspect the WING components: • Lower skin panel span wise joint (SSI 57-21-30)

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 5. PROGRAMA DE PREVENCION Y CONTROL DE LA CORROSION

Fecha de Efectividad: 05-Abr-10 Page: 5 -1- 10 .

"CORROSION PREVENTION & CONTROL PROGRAM CPCP"

Número de Tarea Task Number 57-21-00-210-C20-A00 57-21-00-210-C21-A00 57-21-00-210-C22-A00 57-21-00-210-C23-A00 57-21-00-210-C24-A00 57-21-00-210-C25-A00

57-22-00-220-C01-A00

57-23-00-210-C01-A00 57-23-00-220-C01-A00 57-24-00-210-C02-A00 57-24-00-210-C03-A00 57-24-00-210-C04-A00 57-24-00-210-C05-A00

Grupo Group CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

Tipo Type

Cat. Cat.

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

DET

CPCP

GVI

CPCP

DET

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

-

60 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

-

120 MOS

EMB-145EU EMB-145EP EMB-145ER EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-145XR

-

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

GVI

CPCP

Externally inspect the WING components: • Upper skin/rib attachment (SSI 57-25-55)

96 MOS

60 MOS

ALL

GVI

CPCP Internally inspect the WING components: • Ribs, main box (SSI 57-25-53)

-

120 MOS

EMB-145EU EMB-145EP EMB-145ER EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-135ER EMB-135LR EMB-135KE EMB-135KL

GVI

CPCP

-

120 MOS

ALL

GVI

CPCP

-

120 MOS

ALL

-

15 MOS

ALL

-

30 MOS

ALL

-

15 MOS

ALL

57-25-00-210-C03-A00

CORROSION PROGRAM

57-26-00-220-C02-A00

60 MOS

60 MOS

CORROSION PROGRAM

57-26-00-220-C01-A01

-

96 MOS

57-25-00-210-C02-A00

57-26-00-220-C01-A00

Internally inspect the WING components: • Spar 2/wing stub attachments (SSI 57-23-48) Externally inspect the WING components: • Spar 2, web and stiffeners (SSI 57-23-45) Externally inspect the WING components: • Spar 3, web and stiffeners (SSI 57-24-49) Internally inspect the WING components: • Spar 3, web and stiffeners (SSI 57-24-49) Externally inspect the WING components: • Spar 3, web cutouts (SSI 5724-51) Internally inspect the WING components: • Spar 3, web cutouts (SSI 5724-51)

Efectividad Effect.

CPCP

GVI

57-25-00-210-C05-A00

Internally inspect the WING components: • Spar 1, web and stiffeners (SSI 57-22-40)

Intervalo Interval

EMB-145EU EMB-145EP EMB-145ER EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-135ER EMB-135LR EMB-135KE EMB-135KL

57-25-00-210-C01-A00

CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

Externally inspect the WING components: • Upper skin panel span wise joint (SSI 57-21-31) Externally inspect the WING components: • Lower skin access holes (SSI 57-21-32) Externally inspect the WING components: • Gravity fuel hole (SSI 57-2135) Externally inspect the WING components: • Lower skin/wing stub attachment (SSI 57-21-38) Internally inspect the WING components: • Gravity fuel hole (SSI 57-2135) Internally inspect the WING components: • Upper skin/spar attachment (SSI 57-21-37)

Umbral Thrsld.

Externally inspect the WING components: • Lower skin/rib attachment (SSI 57-25-54)

CORROSION PROGRAM

57-25-00-210-C04-A00

Descripción / Description

DET

CPCP

DET

CPCP

DET

CPCP

Internally inspect the WING components: • Lower skin/rib attachment (SSI 57-25-54) Internally inspect the WING components: • Upper skin/rib attachment (SSI 57-25-55) Internally inspect the WING components: • FWD & aft side brace fittings – MLG (SSI 57-26-56) Internally inspect the WING components: • FWD & aft side brace fittings – MLG (SSI 57-26-56) Internally inspect the WING components: • Lower Bearing Cap (SSI 5726-94)

Applicable to aircraft Pre-Mod. SB 145-320063. Applicable to aircraft Post-Mod. SB 145-320063. Applicable to aircraft Pre-Mod. SB 145-320063.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 5. PROGRAMA DE PREVENCION Y CONTROL DE LA CORROSION

Fecha de Efectividad: 05-Abr-10 Page: 5 -1- 11 .

"CORROSION PREVENTION & CONTROL PROGRAM CPCP"

Número de Tarea Task Number

57-26-00-220-C02-A01

57-26-00-220-C03-A00 57-26-00-220-C03-A01 57-26-00-220-C04-A00 57-26-00-220-C04-A01 57-28-00-210-C01-A00 57-28-00-210-C02-A00 57-28-00-210-C03-A00

57-28-00-210-C06-A00

57-28-00-210-C07-A00 57-28-00-210-C08-A00 57-28-00-210-C09-A00 57-28-00-210-C10-A00 57-28-00-210-C11-A00 57-28-00-210-C13-A00 57-28-00-210-C14-A00 57-28-00-210-C15-A00 57-28-00-220-C01-A00 57-28-00-220-C03-A00 57-28-00-220-C05-A00 57-28-00-220-C07-A00 57-28-00-220-C09-A00 57-28-00-220-C11-A00

Grupo Group

CORROSION PROGRAM

CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

Tipo Type

Cat. Cat.

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

GVI

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

DET

CPCP

Descripción / Description

Internally inspect the WING components: • Lower Bearing Cap (SSI 5726-94)

Internally inspect the WING components: • Aft upper trunnion (SSI 57-2695). Internally inspect the WING components: • Aft upper trunnion (SSI 57-2695). Internally inspect the WING components: • Fwd upper trunnion (SSI 5726-96). Internally inspect the WING components: • Fwd upper trunnion (SSI 5726-96). Externally inspect the WING components: • Lower skin, torque box (SSI 57-28-58) Externally inspect the WING components: • Spar attachment, torque box (SSI 57-28-57) Externally inspect the WING components: • Spar attachment, torque box (SSI 57-28-57) Externally inspect the WING components: • Attachment lugs aileron (SSI 57-28-66) Externally inspect the WING components: • Flap actuator attachment fittings (SSI 57-28-67) Internally inspect the WING components: • Lower skin, torque box (SSI 57-28-58) Internally inspect the WING components: • Upper skin, torque box (SSI 57-28-61) Internally inspect the WING components: • Spar attachment, torque box (SSI 57-28-57) Internally inspect the WING components: • Upper skin, torque box (SSI 57-28-61) Internally inspect the WING components: • Lower skin, torque box (SSI 57-28-58) Internally inspect the WING components: • Tracks/ribs attachment, torque box (SSI 57-28-62) Externally inspect the WING components: • Lower skin, torque box (SSI 57-28-58) Externally inspect the WING components: • Spar attachment, torque box (SSI 57-28-57) Externally inspect the WING components: • Flap track, torque box (SSI 57-28-59) Externally inspect the WING components: • Tracks/rib attachment, torque box 3 (SSI 57-28-65) Externally inspect the WING components: • Attachment actuator lugs, inboard/outboard spoilers (SSI 57-28-70) Internally inspect the WING components: • Tracks/rib attachment, torque box 3 (SSI 57-28-65) Internally inspect the WING components: • Ribs, torque box (SSI 57-2860)

Applicable to aircraft Post-Mod. SB 145-320063. NOTE 2: If corrosion is detected on the lower bearing cap internal surface, perform internal inspection on the corresponding upper trunnion bearing surface. Applicable to aircraft Pre-Mod. SB 145-320063. Applicable to aircraft Post-Mod. SB 145-320063. Applicable to aircraft Pre-Mod. SB 145-320063. Applicable to aircraft Post-Mod. SB 145-320063.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

30 MOS

ALL

-

15 MOS

ALL

-

60 MOS

ALL

-

15 MOS

ALL

-

60 MOS

ALL

-

30 MOS

ALL

48 MOS

30 MOS

ALL

96 MOS

60 MOS

ALL

-

60 MOS

EMB-145EU EMB-145EP EMB-145ER EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-145XR

96 MOS

60 MOS

ALL

-

60 MOS

ALL

96 MOS

60 MOS

ALL

-

120 MOS

ALL

-

120 MOS

ALL

-

60 MOS

ALL

-

120 MOS

ALL

-

30 MOS

ALL

72 MOS

30 MOS

ALL

96 MOS

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

-

120 MOS

ALL

96 MOS

60 MOS

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 5. PROGRAMA DE PREVENCION Y CONTROL DE LA CORROSION

Fecha de Efectividad: 05-Abr-10 Page: 5 -1- 12 .

"CORROSION PREVENTION & CONTROL PROGRAM CPCP"

Número de Tarea Task Number 57-28-00-220-C12-A00 57-41-00-210-C01-A00 57-42-00-210-C01-A00 57-42-00-220-C01-A00 57-43-00-210-C01-A00 57-50-00-220-C01-A00 57-50-00-220-C02-A00 57-52-00-210-C01-A00 57-52-00-220-C01-A00 57-53-00-210-C01-A00 57-53-00-210-C02-A00

57-61-00-210-C01-A00

57-61-00-210-C02-A00 57-70-00-210-C01-A00 57-70-00-210-C02-A00

Grupo Group CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM

Tipo Type

Cat. Cat.

DET

CPCP

GVI

CPCP

GVI

CPCP

DET

CPCP

GVI

CPCP

DET

CPCP

DET

CPCP Externally inspect the FLAP components: • Tracks, flaps (SSI 57-50-80)

GVI DET GVI GVI

GVI

GVI GVI GVI

Descripción / Description Externally inspect the WING components: • Ribs, torque box (SSI 57-2860) Externally inspect the WING LEADING EDGE components: • Wing leading edge 1 skin (SSI 57-41-94) Externally inspect the WING LEADING EDGE components: • Wing leading edge 2 skin (SSI 57-42-95) Externally inspect the WING LEADING EDGE components: • Wing leading edge 2 bottom skin at connections to lower rear girder & wing lower spar cap (SSI 57-42-97) Externally inspect the LEADING EDGE components: • Wing leading edge 3 skin (SSI 57-43-96) Externally inspect the FLAP components: • Tracks/rib attachment, flaps(SSI 57-50-77)

Externally inspect the FLAP components: • Pin and actuator lugs, inboard flap (SSI 57-52-75) Externally inspect the FLAP components: • Fitting tip spar, inboard flap CPCP (SSI 57-52-73) Externally inspect the FLAP components: • Pin and actuator lugs, CPCP outboard flap (SSI 57-53-84) Externally inspect the FLAP components: • Center ribs attachment, CPCP outboard flap (SSI 57-53-87) CPCP

CPCP

Externally inspect the AILERON components: • Hinges attachment, aileron (SSI 57-61-89)

Externally inspect the AILERON components: • Spar cap, aileron (SSI 5761-91) Externally inspect the SPOILER components: • Hinges attachment, CPCP spoilers (SSI 57-70-92) Externally inspect the SPOILER components: • Actuator attachment, CPCP spoilers (SSI 57-70-93) CPCP

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

96 MOS

60 MOS

ALL

48 MOS

30 MOS

ALL

48 MOS

30 MOS

ALL

-

30 MOS

ALL

48 MOS

30 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

ALL

96 MOS

60 MOS

EMB-145EU EMB-145EP EMB-145ER EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-145XR

96 MOS

60 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 6. REQUERIMIENTOS DE INSPECCION POR ZONAS

Fecha de Efectividad: 05-Abr-10 Page: 6 -1- 1 .

"ZONAL INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

32-Z711-213-001-A00

ZONAL

GVI

-

32-Z721-213-001-A00

ZONAL

GVI

-

52-Z811-213-001-A00

ZONAL

GVI

-

52-Z811-214-001-A00

ZONAL

GVI

-

Descripción / Description

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

C

ALL

-

C

ALL

External General Visual Inspection ZONES ZONES 711/713/714/113/114/115/116 External General Visual Inspection ZONES ZONES 721/731/722/732/532/632

NLG AND DOORS NOTE: EWIS MLG AND DOORS NOTE: EWIS

External General Visual Inspection ZONE 811

MAIN DOOR

-

2C

ALL

Internal General Visual Inspection ZONE 811

MAIN DOOR ACCESS 811AW/BW/CW/DW/EW/FW/GW/HW/J W/KW/LW/MW/NW/PW/QW/RW/SW/T W/UW/VW

-

C

ALL

-

C

ALL

52-Z811-214-002-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONE 811

MAIN DOOR Only aircraft equipped with side hinged main door model. ACCESS 811AAW/ABW/ACW/ADW/AEW/XW/Y W/ZW

52-Z812-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 812/822

ESCAPE HATCH

-

4C

ALL

-

4C

ALL

52-Z812-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 812/822

ESCAPE HATCH ACCESS 812AW 822AW

52-Z813-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONE 813

BAGAGGE DOOR

-

2C

ALL

-

C

ALL

52-Z813-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONE 813

BAGAGGE DOOR ACCESS 813AW

52-Z821-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONE 821

SERVICE DOOR

-

2C

ALL

-

C

ALL

52-Z821-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONE 821

SERVICE DOOR ACCESS 821AW/ BW/CW

53-Z111-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONE 111

RADOME

-

2C

ALL

53-Z111-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONE 111. Access 111.

RADOME

-

2C

ALL

53-Z113-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 113/114

FW FUSELAGE

-

2C

ALL

53-Z113-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 113. Access 113AZ 113BZ 113CZ 113DL 113EL 114AZ 114BZ 114CR.

FW FUSELAGE

-

2C

ALL

53-Z114-214-001-A00

ZONAL

GVI

Internal General Visual Inspection ZONE 114

ACCESS 114CR NOTE: EWIS

2C

ALL

53-Z123-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 123/124

FW FUSELAGE

-

2C

ALL

Internal General Visual Inspection ZONES 121/122/123/124. Access 123BL, 221AF/BF/CF/DF/EF/FF/GF, 222AF/BF/CF/DF/EF/GF

FW FUSELAGE NOTE: EWIS

-

2C

ALL

53-Z123-214-001-A00

ZONAL

GVI

-

53-Z131-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 131/132

CENTER FUSELAGE

-

2C

ALL

-

Internal General Visual Inspection ZONES 131/132. Access 231AF 231BF 231CF 231DF 231EF 231FF 231GF 231HF 232AF 232BF 232CF 232DF.

CENTER FUSELAGE NOTE: EWIS

-

C

ALL

53-Z131-214-001-A00

ZONAL

GVI

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 6. REQUERIMIENTOS DE INSPECCION POR ZONAS

Fecha de Efectividad: 05-Abr-10 Page: 6 -1- 2 .

"ZONAL INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

53-Z141-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 141/142.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

CENTER FUSELAGE

-

2C

ALL

CENTER FUSELAGE NOTE: EWIS

-

2C

ALL

Descripción / Description

53-Z141-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 141/142. Access 231GF 231HF 241AF 241BF 241CF 241DF 241EF 242AF 242BF 242CF 242DF 251BF

53-Z151-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection 251AF/BF/CF/DF/EF/FF/GF/HF/252AF/BF/ CF/DF

CENTER FUSELAGE NOTE: EWIS

-

2C

EMB-145EU EMB-145EP EMB145ER EMB-135ER

53-Z151-214-002-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 151/152/153/154. Access 251AF 251BF 251CF 251DF 251/EF 251FF 251GF 251HF 252AF 252BF 252DF 252EF.

CENTER FUSELAGE NOTE: EWIS

-

2C

EMB-145LR EMB-145LU EMB145MR EMB-145MP EMB-145MK EMB-145XR EMB-135LR EMB135KE EMB-135KL

CENTER FUSELAGE NOTE: EWIS

2C

EMB-145LR EMB-145LU EMB145MR EMB-145MP EMB-145MK EMB-145XR EMB-135LR EMB135KE EMB-135KL

2C

EMB-145EU EMB-145EP EMB-145ER EMB-135ER

53-Z155-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 155/156. Access 155BZ/CZ DZ/EZ/FZ/GZ/KZ/LZ/MZ/NZ/QZ156BZ/CZDZ/EZ/FZ/GZ/KZ/LZ/ MZ/NZ/QZ192AL192BR

53-Z155-214-002-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 155/156; ACCESS 155BZ/CZDZ/EZ/FZ/GZ/KZ/LZ/MZ/QZ156BZ/CZDZ/EZ/FZ/GZ/ KZ/LZ/MZ/QZ192AL 192BR

NOTE: EWIS

53-Z161-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 161/162. Access 251JF/HF 252DF 261AF/BF/ CF/DF 262AF/BF/ CF

CENTER FUSELAGE NOTE: EWIS

-

2C

ALL

53-Z171-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 171/172

REAR FUSELAGE

-

C

ALL

-

Internal General Visual Inspection ZONES 171/172. Access 271AF 271BF 271CF 271DF 271EF 271FF 272AF 272BF 272CF 272DR

REAR FUSELAGE NOTE: EWIS

-

C

ALL

2C

EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-145EU EMB-145EP EMB-145ER EMB-135LR EMB-135KE EMB-135KL EMB-135ER

53-Z171-214-001-A00

53-Z191-213-001-A00

ZONAL

ZONAL

GVI

GVI

-

External General Visual Inspection ZONES 191

WING TO FUSELAGE ATTACHMENT FAIRING

-

-

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 6. REQUERIMIENTOS DE INSPECCION POR ZONAS

Fecha de Efectividad: 05-Abr-10 Page: 6 -1- 3 .

"ZONAL INSPECTION REQUIREMENTS" Número de Tarea Task Number

53-Z191-214-001-A00

Grupo Group

ZONAL

Tipo Type

GVI

Cat. Cat.

Umbral Thrsld.

Descripción / Description

WING TO FUSELAGE ATTACHMENT FAIRING NOTE: EWIS

-

Internal General Visual Inspection ZONES 191/192/193/194/195

NOTE: EWIS

-

Intervalo Interval

Efectividad Effect.

2C

EMB-145LR EMB-145LU EMB-145MR EMB-145MP EMB-145MK EMB-135LR EMB-135KE EMB-135KL

2C

EMB-145EU EMB-145EP EMB-145ER EMB-135ER

53-Z191-214-002-A00

ZONAL

GVI

-

Internal General Visual Inspection ACCESS 191ZB 192LB 193ABB 194ER 195EL

53-Z213-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 213/214

FW FUSELAGE

-

2C

ALL

53-Z213-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 213/214/215/216. Access 113AZ 113BZ 113CZ 114AZ 114BZ

FW FUSELAGE NOTE: EWIS

-

2C

ALL

53-Z223-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 223/224

FW FUSELAGE

-

2C

ALL

FW FUSELAGE NOTE: EWIS

-

2C

ALL

53-Z223-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 221/222/223/224. Access 223AZ/BZ/CLW/DLW/ELW/FLW/GZ/HZ/IZ/JLW/KLW/LZ/MZ/NZ /OZ/PZ/QZ/RZ/SZ/TZ/UZ224CRW/DRW/ERW/FRW/GZ/HZ/JR W/KRW/224MZ/NZ

53-Z225-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 225/226

FW FUSELAGE

-

4C

ALL

Internal General Visual Inspection ZONES 225/226. Access 225ALC/BLC/CTC, 226ARC, 226BRC.

FW FUSELAGE NOTE: Perform at the opportunity of CPCP task 53-12-00-220-C01-A00 accomplishment.

-

4C

ALL

53-Z225-214-001-A00

ZONAL

GVI

-

53-Z231-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 231/232

CENTER FUSELAGE

-

2C

ALL

Internal General Visual Inspection ZONES 231/232. Access 231ALW 231BLW 231CLW 241ALW 241DLW 242ARW 242BRW 242DRW

CENTER FUSELAGE

-

2C

ALL

53-Z231-214-001-A00

ZONAL

GVI

-

53-Z233-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 233/234

CENTER FUSELAGE

-

2C

ALL

CENTER FUSELAGE

-

4C

ALL

53-Z233-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 233/234. Access 233ALC 233BLC 233CLC 234ARC 243ALC

53-Z241-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 241/242

CENTER FUSELAGE

-

4C

ALL

53-Z241-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 241/242. Access 231BLW 231CLW 241ALW/ BLW/CLW/ DLW/ELW 242ARW/ BRW/CRW/ DRW/ERW 251ALW 251ELW 252ARW 252ERW

CENTER FUSELAGE

-

3C

ALL

53-Z243-213-003-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 243/244

CENTER FUSELAGE

-

4C

ALL

-

Internal General Visual Inspection ZONES 243/244. Access 243ALC/ BLC/CLC/ DLC 253ALC

CENTER FUSELAGE

-

4C

ALL

53-Z243-214-001-A00

ZONAL

GVI

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 6. REQUERIMIENTOS DE INSPECCION POR ZONAS

Fecha de Efectividad: 05-Abr-10 Page: 6 -1- 4 .

"ZONAL INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

53-Z251-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 251/252 Internal General Visual Inspection ZONES 251/252. Access 241CLW 251ALW BLW/CLW/ DLW/ELW/ FLW/GLW 252ARW/ BRW/CRW/ DRW/ERW/ FRW/GRW 261ALW/ CLW 262ARW/ CRW

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

CENTER FUSELAGE

-

4C

ALL

CENTER FUSELAGE

-

3C

ALL

Descripción / Description

53-Z251-214-001-A00

ZONAL

GVI

-

53-Z253-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 253/254

CENTER FUSELAGE

-

4C

ALL

CENTER FUSELAGE

-

4C

ALL

53-Z253-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 253/254. Access 253ALC/ BLC/CLC/ DLC/ELC 263ALC

53-Z261-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 261/262

CENTER FUSELAGE

-

4C

ALL

53-Z261-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 261/262. Access 261ALW/BLW/CLW/DLW 262ARW/BRW/CRW/DRW

CENTER FUSELAGE

-

2C

ALL

53-Z263-213-002-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 263/264

CENTER FUSELAGE

-

4C

ALL

Internal General Visual Inspection ZONES 263/264. Access 263ALC/ BLC

CENTER FUSELAGE NOTE: EWIS

-

4C

ALL

53-Z263-214-001-A00

ZONAL

GVI

-

53-Z271-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 271/272

REAR FUSELAGE

-

C

ALL

Internal General Visual Inspection ZONES 271/272. Access 271ALW/BLW 272ARW/BRW/CRW/DR. External General Visual Inspection ZONES 273/274. Access 322. Internal General Visual Inspection ZONES 273/274. Access 273ATC 273BTC 273CTC. Internal General Visual Inspection ZONES 275/276. Access 272DR.

REAR FUSELAGE NOTE: EWIS

-

2C

ALL

REAR FUSELAGE

-

4C

ALL

NOTE: EWIS

-

2C

ALL

REAR FUSELAGE NOTE: EWIS

-

2C

ALL

53-Z271-214-002-A00

ZONAL

GVI

-

53-Z273-213-002-A00

ZONAL

GVI

-

53-Z273-214-001-A00

ZONAL

GVI

-

53-Z275-214-001-A00

ZONAL

GVI

-

53-Z311-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 311/312

REAR FUSELAGE II

-

2C

ALL

Internal General Visual Inspection ZONES 311/312. Access 312AR

REAR FUSELAGE II

-

2C

ALL

53-Z311-214-001-A00

ZONAL

GVI

-

53-Z313-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONE 313

TAIL CONE FAIRING

-

C

ALL

Internal General Visual Inspection ZONE 313. Access 313 313AL 313BL 313CL 313DR 313GR 312AR

TAIL CONE FAIRING NOTE: EWIS

-

C

ALL

53-Z313-214-001-A00

ZONAL

GVI

-

54-Z414-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 414/424

ENGINE PYLONS

-

C

ALL

ENGINE PYLONS NOTE: EWIS

-

C

ALL

-

2C

ALL

-

2C

ALL

-

2C

ALL

54-Z414-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 414/424. Access 414AB/BB/CB/DB/EB/FT/GT 424AB 424BB 424CB 424DB 424EB 424FT 424GT.

55-Z321-213-001-A00

ZONAL

GVI

-

External General Visual Inspection

55-Z321-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection

55-Z324-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 324/325/321/322/323.

ACCESS 321; 322; 323; 337AZ; 337BZ; 337CZ VERTICAL STABILIZER AND RUDDERS

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 6. REQUERIMIENTOS DE INSPECCION POR ZONAS

Fecha de Efectividad: 05-Abr-10 Page: 6 -1- 5 .

"ZONAL INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

55-Z324-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 324/325/321/322/323. Access 324AL 324BL 324CL 324DL 324EL 324FR 325AL 325BL 325CL 325DL 325EL 325FL 325FR 325GR 325HR 325JR 325KR 325LR

VERTICAL STABILIZER AND RUDDERS NOTE: EWIS

-

2C

ALL

55-Z326-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONE 326

VERTICAL STABILIZER AND RUDDERS

-

2C

ALL

55-Z326-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONE 326. Access 326AL; 326BL; 326CL; 326DL; 326EL; 326FL; 326GL; 326HL; 327AL; 327BL; 327CL; 27DL; 327ER; 327FR; 327GR; 327HR

VERTICAL STABILIZER AND RUDDERS

-

2C

ALL

55-Z333-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 333/334/331/332

VERTICAL STABILIZER AND RUDDERS

-

2C

ALL

55-Z333-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 333/334/331/332. Access 333AB 333BB 333CB 333DL 334AB 334BB 334CB 334DR

VERTICAL STABILIZER AND RUDDERS

-

2C

ALL

55-Z335-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 335/336

HORIZONTAL STABILIZER AND ELEVATOR

-

2C

ALL

55-Z335-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 335/336. Access 335AB 335BB 335CB 335DB 335EB 335FB 335GB 335HB 336AB 336BB 336CB 336DB 336EB 336FB 336GB 336HB.

HORIZONTAL STABILIZER AND ELEVATOR

-

2C

ALL

57-Z511-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 511/611/512/612/513/613

WING LEADING EDGE

-

C

ALL

57-Z511-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 511/611/512/612/513/613. ACCESS 511 512 513 611 612 613 561 661 191EL 191FR

WING LEADING EDGE NOTE: EWIS

-

2C

ALL

57-Z531-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 531/631

WING

-

2C

ALL

57-Z531-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 531/631. Access 531AB 531BB 531CB 531DB 631AB 631BB 631CB 631DB

WING NOTE: EWIS

-

2C

ALL

57-Z532-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 532/632

WING

-

2C

ALL

Internal General Visual Inspection ZONES 532/632. Access 532AB 532BB 632AB 632BB.

WING NOTE: EWIS

-

2C

ALL

Descripción / Description

57-Z532-214-001-A00

ZONAL

GVI

-

57-Z541-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 541/641

WING

-

2C

ALL

-

Internal General Visual Inspection ZONES 541/641. Access 541AB/BB/CB/DB/EB/FT 541GB 641AB/BB/CB/DB/EB/FT 641GB

WING NOTE: EWIS

-

2C

ALL

2C

EMB-145LR EMB-145LU EMB145MR EMB-145MP EMB-145MK EMB-145EU EMB-145EP EMB145ER EMB-135LR EMB-135KE EMB-135KL EMB-135ER

57-Z541-214-001-A00

57-Z551-213-001-A00

ZONAL

ZONAL

GVI

GVI

-

External General Visual Inspection ZONES 551/651/561/661

WING

-

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 6. REQUERIMIENTOS DE INSPECCION POR ZONAS

Fecha de Efectividad: 05-Abr-10 Page: 6 -1- 6 .

"ZONAL INSPECTION REQUIREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Descripción / Description

Intervalo Interval

Efectividad Effect.

WING NOTE: EWIS

-

2C

EMB-145LR EMB-145LU EMB145MR EMB-145MP EMB-145MK EMB-145EU EMB-145EP EMB145ER EMB-135LR EMB-135KE EMB-135KL EMB-135ER

57-Z551-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 551/651/561/661. Access 551AB 551BB/ 551CB 551DB/ 551EB 551FT/ 651AB 651BB/ 651CB 651DB 651EB 651FT 561 661

57-Z571-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 571/671/5711/6711/5712/6712/5713/6713

WING TRAILING EDGE

-

2C

ALL

57-Z571-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 571/671/5711/6711/5712/6712/5713/6713. Access 5711 6711 5712 5713 6712 6713 571AB/BB 671AB/BB

WING TRAILING EDGE NOTE: EWIS

-

2C

ALL

57-Z572-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 572/672/5721/6721/5722/6722

WING TRAILING EDGE

-

2C

ALL

57-Z572-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 572/672/5721/6721/5722/6722. Access 5721 5722 6721 6722 572AB/BB 672AB/BB

WING TRAILING EDGE NOTE: EWIS

-

2C

ALL

57-Z573-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 573/673/5731/6731/5732/6732

WING TRAILING EDGE

-

2C

ALL

57-Z573-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 573/673/5731/6731/5732/6732. Access 5731 5732 6731 6732 573AT 673AT

WING TRAILING EDGE NOTE: EWIS

-

2C

ALL

71-Z411-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 411/412/413 AND 421/422/423

POWER PLANT

-

C

ALL

71-Z411-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 411/412/413/415 AND 421/422/423/425. Access 411 412 413 421 422 423

POWER PLANT NOTE: EWIS

-

C

ALL

78-Z416-213-001-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 416/426

-

C

ALL

78-Z416-213-001-A01

ZONAL

GVI

-

External General Visual Inspection. ZONES 416/426

2C

ALL

-

Internal General Visual Inspection ZONES 416/426. Access 416AB/BB/CB/DB/EB/FB/GB/HT/IZ/JT/ KT/LT/MT/NT/PR/QL/RR/SL/TR/UL/VZ /XZ/WZ/YZ 416ZZ 426AB/BB/CB/DB/EB/FB/GB/HT/JT/K T/LT/MT/NT/PR/IZ/QL/RR/SL/TR/UL/V Z/XZ/WZ/YZ 426ZZ

C

ALL

78-Z416-214-001-A00

ZONAL

GVI

Applicable to aircraft WITH thrust reversers installed. THRUST REVERSER MODULE NOTE: For aircraft without Thrust Reversers only Applicable to aircraft WITH thrust reversers installed. THRUST REVERSER MODULE NOTE: EWIS

-

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 7. REQUERIMIENTOS DE MANTENIMIENTO POR CERTIFICACION

Fecha de Efectividad: 05-Abr-10 Page: 7 -1-1 .

"CERTIFICATION MAINTENANCE REQUIEREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

Check also Rudder System Auto Shutoff Logical Circuit, Electrical Hardware and related EICAS Messages with both systems ON, then one system at a time. In addition, visually check microswitches. UNDER CTA/FAA CERTIFICATIONS

-

2500 FH

ALL

UNDER CTA/FAA CERTIFICATIONS

-

5000 FH

ALL

UNDER CTA/FAA CERTIFICATIONS

-

10000 FH

ALL

UNDER CTA/FAA CERTIFICATIONS

-

5000 FH

ALL

UNDER CTA/FAA CERTIFICATIONS

-

5000 FH

ALL

UNDER CTA/FAA CERTIFICATIONS

-

5000 FH

ALL

Operationally Check Air/Ground System

UNDER CTA/FAA CERTIFICATIONS

-

500 FH

ALL

-

1000 FH

ALL

Descripción / Description

Operationally Check Rudder Pedals Auto Shutoff and Rudder Manual Shutoff Functions

27-25-00-710-001-A00

SYSTEMS

OPC

CMR

27-31-05-220-001-A00

SYSTEMS

DVI

CMR Inspect (Detailed Inspection) Servo Tab Failsafe Actuation Link

27-62-00-720-001-A00

SYSTEMS

FNC

CMR

30-11-00-720-001-A00

SYSTEMS

FNC

30-12-00-720-001-A00

SYSTEMS

FNC

30-21-00-720-001-A00

SYSTEMS

FNC

32-63-00-710-001-A00

SYSTEMS

OPC

Functionally Check G. Spoiler/Speed Brake Valves, Control Circuit and Associated Messages Functionally Check Pressure Sensors of the Wing Thermal AntiCMR Icing System (Bench Test) Functionally Check Pressure Sensors of the Horizontal CMR Stabilizer Thermal Anti-Icing System (Bench Test) Functionally Check Pressure Sensors of the Engine Thermal CMR Anti-Icing System (Bench Test) CMR

78-33-00-710-001-A00

SYSTEMS

OPC

CMR

Operationally Check Air/Ground Input Signal to Thrust Reverser System

Applicable to aircraft WITH thrust reversers installed. UNDER CTA/FAA CERTIFICATIONS

78-33-00-710-002-A00

SYSTEMS

OPC

CMR

Operationally Check Wheel Speed Input Signal to Thrust Reverser System

Applicable to aircraft WITH thrust reversers installed. UNDER CTA/FAA CERTIFICATIONS

-

1000 FH

ALL

78-33-01-710-001-A00

SYSTEMS

OPC

CMR

Operationally Check Isolation Control Unit

UNDER CTA/FAA CERTIFICATIONS

-

1000 FH

ALL

Operationally Check Thrust Reverser Indicating System

Applicable to aircraft WITH thrust reversers installed. UNDER CTA/FAA CERTIFICATIONS

-

10000 FH

ALL

78-34-00-710-001-A00

SYSTEMS

OPC

CMR

F-GAC-01 SEP-07

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components

Page: 8-1-1

CHAPTER 27 – FLIGHT CONTROLS DESCRIPCIÓN Flap drive Motor Unit

NÚMERO DE PARTE 363250-1003 (*)

PROVEEDOR Bertea Control

LIMITE DE VIDA 15000 FH

EFECTIVIDAD EMB-145 (ALL)

(*) NOTE: This life limit is aplicable “only” for the motors with serial numbers 00101, 00102, 00103, 00104, 00105, 00106, 00107, 00108, 00109, 00110.

CHAPTER 32 – LANDING GEAR DESCRIPCIÓN

Leg strut left

Leg strut right

NOT A N/P

N/P

NÚMERO DE PARTE 2309-2006-001 23-09-2006-501 2309-3006-503 2309-2006-601 2309-2015-001 2309-2015-601 2309-3006-501 2309-3006-503 2309-3006-505 2309-3006-601 2309-4006-501 2309-4006-503 2309-2006-002 2309-2006-502 2309-2006-504 2309-2006-602 2309-2015-002 2309-2015-602

EU/EP/ER 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

LIMITE DE VIDA EMB-145 MP/MK/MR LR/LU 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

XR

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

F-GAC-01 SEP-07

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components DESCRIPCIÓN

NOT A

NÚMERO DE PARTE EU/EP/ER

Leg strut right (Continued)

N/P

Trunnion axle Shock absorver attachment Main side strut attachement

N/P N/P

Trainling arm axle (left)

N/P

Training arm axle (right)

N/P

Training arm

N/P

2309-3006-502 2309-3006-504 2309-3006-506 2309-3006-602 2309-4006-502 2309-4006-504 2309-2025-001 2309-3025-001 2309-2032-001 2309-2032-003 2309-2032-005 2309-3032-001 2309-3032-003 2309-3032-005 2309-2055-001 2309-2055-003 2309-3055-001 2309-2055-0022309-2055-004 2309-3055-002 2309-2009-001 2309-2009-003 2309-2009-503 2309-2009-505 2309-2009-507 2309-2009-601 2309-2009-603 2309-2009-605 2309-2009-607

Page: 8-1-2

LIMITE DE VIDA EMB-145 MP/MK/MR LR/LU 60000 (**) 60000 (**) 60000 (**) 60000 (**)

XR

60000 (**) 60000 (**) 60000 (**)

60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**)

60000 (**) 60000 (**)

60000 (**) 60000 (**)

60000 (**) 60000 (**)

40000 (**) 40000 (**) 40000 (**) 40000 (*) 40000 (**) 40000 (**) 40000 (**) 40000 (**) 40000 (*)

40000 (**) 40000 (**) 40000 (**) 40000 (*) 40000 (**) 40000 (**) 40000 (**) 40000 (**) 40000 (*)

60000 (**) 60000 (**)

60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**)

60000 (**)

60000 (**)

60000 (**)

60000 (**)

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components DESCRIPCIÓN

NOT A

NÚMERO DE PARTE 2309-2009-609 2309-2009-611 2309-2009-613 2309-2009-615 2309-2009-617 2309-2038-001 2309-2038-003 2309-2038-005 2309-2038-007 2309-2038-601 2309-2038-603 2309-2038-605 2309-2038-607 2309-2038-609 2309-2038-611 2309-2038-613 2309-3009-501 2309-3009-503 2309-3009-505 2309-3009-507 2309-3009-601 2309-3009-603 2309-3009-605 2309-4009-501 2309-4009-503 2309-4009-505 2309-4009-601 2309-4009-603

EU/EP/ER 40000 (*) 40000 (*) 40000 (*) 40000 (*) 40000 (*) 40000 (**) 40000 (**) 40000 (**) 40000 (*) 40000 (**) 40000 (**) 40000 (*) 40000 (*) 40000 (*) 40000 (*) 40000 (*)

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 8-1-3

LIMITE DE VIDA EMB-145 MP/MK/MR LR/LU 40000 (*) 40000 (*) 40000 (*) 40000 (*) 40000 (*) 40000 (**) 40000 (**) 40000 (**) 40000 (**) 40000 (**) 40000 (*) 40000 (**) 40000 (**) 40000 (*) 40000 (*) 40000 (*) 40000 (*) 40000 (*) 40000 (**) 40000 (**) 40000 (*) 40000 (*) 40000 (**) 40000 (*) 40000 (*)

XR

10000 (**) 40000 (*) 40000 (*) 40000 (*) 10000 (**)

F-GAC-01 SEP-07

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components DESCRIPCIÓN

NOT A

Wheel axle

N/P

Pívot

N/P

Cardan Joint

N/P

MLG SHOCK ABSORBER ELEB Piston tube Cylinder

N/P N/P

Bearing cap

N/P

MLG SECONDARY SIDE STRUT ELEB Upper secondary side strut

N/P

Lower secondary side strut

N/P

Cardan Sahft (axle) Bolt Pivot pin Spring

N/P N/P N/P N/P N/P

NÚMERO DE PARTE 2309-2040-001 2309-3040-001 2309-2050-001 2309-2050-003 2309-2050-601 2309-2048-001 2309-2048-003 2309-2048-005

EU/EP/ER 60000 (**) 60000 (**) 60000 (**) 60000 (**) 15760 (**) 35365 (**) 48948 (**)

Page: 8-1-4

LIMITE DE VIDA EMB-145 MP/MK/MR LR/LU 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 15760 (**) 15760 (**) 35365 (**) 35365 (**) 48948 (**) 48948 (**)

2309-2058-001 2309-2056-001 2309-2056-003 2309-2056-005 2309-2066-001 2309-2082-001

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

2309-2609-001 2309-2611-001 2309-2611-003 2309-2603-001 2309-2624-001 2309-2618-001 2309-2621-001 2309-2626-001 2309-2613-001 2309-2651-001 2309-2651-003 2309-2651-005

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 20000 (**) 20000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 20000 (**) 20000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 20000 (**) 20000 (**) 60000 (**)

XR 60000 (**) 60000 (**) 60000 (**) 60000 (**) 15760 (**) 35365 (**) 48948 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**)

F-GAC-01 SEP-07

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components DESCRIPCIÓN

NOT A

NÚMERO DE PARTE EU/EP/ER

MLG MAIN SIDE STRUT ELEB Upper main side strut

N/P

Lower main side strut

N/P

Shaft

N/P

Pivot pin

N/P

NLG LEG STRUT LIEBHER Slinding tube

N/P

Wheel axle

N/P

Steering cuff Torque link Torque link pin Torque link central bolt

N/P N/P N/P N/P

Page: 8-1-5

LIMITE DE VIDA EMB-145 MP/MK/MR LR/LU

2309-2503-001 2309-2504-001 2309-2524-001 2309-2511-001 2309-2532-001 2309-2532-003 2309-2532-005 2309-2515-001 2309-3515-001 2309-2516-001 2309-3516-001

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**)

60000 (**)

1170-1401 2233-0201 1170-1402 1170-1403 1170-1431 1170-1432 1170-1433 1170-1434 2233-0202 2233-0230 2233-0231 1170-2301 1170-0301 1170-0001 1170-0002

60000 (**)

60000 (**)

60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

XR

60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**)

60000 (**)

60000 (**)

60000 (**)

60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

F-GAC-01 SEP-07

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components DESCRIPCIÓN

Main fitting

NOT A N/P

Main drag strut attachment pin Pintle pin NLG MAIN DRAG STRUT LIEBHER Main drag strut top stay

N/P N/P N/P

Main drag strut bottom stay Pintle pin

N/P N/P

Hinge point bolt NLG AUXILIARY DRAG STRUT LIEBHER Upper aux drag strut Lower aux. drag strut Hinge point bolt Cardan joint attaching parts Downlock spring

N/P N/P N/P N/P N/P N/P

Auxiliary drag strut

N/P

NÚMERO DE PARTE

Page: 8-1-6

LIMITE DE VIDA EMB-145 MP/MK/MR LR/LU 20000 (**) 20000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

1170-1301 1170-1302 1170-1303 1170-1304 1170-1305 2233-0101 2233-0103 1170-0070 1170-0032

EU/EP/ER 20000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

1172-0501 1172-0601 1172-0201 1172-0007 1172-0037 1172-0001

60000 (**) 60000 (**) 60000 (**) 6000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 6000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 6000 (**) 60000 (**) 60000 (**)

1173-0201 1173-0101 1173-0001 KSL113608V 1173A0300-01 1173A0600-01 1173A0700-01 (***)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 20000 (*) 30901 (**) 60000 (**) 6000 (***)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 20000 (*) 30901 (**) 60000 (**) 6000 (***)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 20000 (*) 30901 (**) 60000 (**) 6000 (***)

XR

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**) 60000 (**)

60000 (**) 6000 (***)

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 8-1-7

NOTE: The column “NOTE” indicates if the P/N is procurable (P) or Non-procurable (N/P) NOTE : (*) The definitive life limits will be based on fatigue tests being concluded. The current status of these fatigue tests assure a minimum of the above flight cycles of safe operation. NOTE : (**) Permanent life limit . NOTE : (***) The life limit is applicable “only” for the Auxiliary Drag Strut with serial numbers SP010-96, SP011-96, SP012-96 and SP013-96.

CHAPTER 35- OXYGEN DESCRIPCION Oxygen Cylinder

NUMERO DE PARTE 176250-50 4441009-050

SUPPLIER B/E AEROSPACE

LIMITE DE VIDA 180 MO 180 MO

EFFECTIVITY ALL

CHAPTER 36-PNEUMATIC DESCRIPCION Low Pressure Bleed-Air Check Valve

NUMERO DE PARTE 816603-1 816603-2

SUPPLIER Hamilton Standard

LIMITE DE VIDA 1600 FH 1600 FH

EFFECTIVITY ALL ALL

LIMITE DE VIDA 2500 FH 2500 FH

EFFECTIVITY ALL ALL

CHAPTER 49-APU DESCRIPCION Non-Silenced APU C-14(APS 500R)Exhaust duct

NUMERO DE PARTE 145-63730-401 145-63730-601

SUPPLIER Embraer

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 8-1-8

CHAPTER 72- ENGINE

DESCRIPTION

ST Nº

P/N

Rolls-Royce AE3007 Engine Model-Life Limit (FC) A1 A1P 20000 20000 19400 19400

Fan Wheel

23058865 23061670

Forwar Fan Blade Retainer

23062491

20000

20000

Fan drive shaft

23058320 23065332 23074382

30000 30000 30000

30000 30000 30000

23064901 23065041 23084156 23050752 23084157 23050753 23065303 23084158 23050754 23071259 23084159 23050735 23065605 23071260 23084160

12500 20000 30000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

12500 20000 30000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

HP Compresor wheels

1st

2nd 3rd

4th

5th

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components

DESCRIPTION

ST Nº

HP Compresor wheels Continued

6th

7th

8th

9th

10th

11th

P/N 23062666 23071261 23071396 23074717 23084161 23062667 23071262 23071397 23074217 23074719 23084162 23084350 23061628 23071263 23074721 23084163 23061629 23071264 23074722 23084164 23061630 23071265 23074723 23084165 23061631 23066231 23074724 23084166

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 8-1-9

Rolls-Royce AE3007 Engine Model-Life Limit (FC) A1 A1P 20000 20000 20000 20000 20000 20000 20000 20000 30000 30000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 30000 30000 30000 30000 20000 20000 20000 20000 20000 20000 30000 30000 20000 20000 20000 20000 20000 20000 30000 30000 20000 20000 20000 20000 20000 20000 30000 30000 20000 20000 20000 20000 20000 20000 30000 30000

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components

DESCRIPTION

ST Nº

P/N

HP Compresor wheels Continued

12th

23061632 23071267 23074725 23084167 23061633 23071268 23074213 23074726 23084168 23084283 23061634 23071269 23074214 23084169 23084284

13th

14th

Compresor cone shaft

HP turbine wheels

15th

1st

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 8-1-10

Rolls-Royce AE3007 Engine Model-Life Limit (FC) A1 A1P 20000 20000 20000 20000 20000 20000 30000 30000 20000 20000 20000 20000 20000 20000 20000 20000 30000 30000 30000 30000 20000 20000 20000 20000 20000 20000 30000 30000 30000 30000

23050728 23070729

7500 7500

23073282 23076016 23076017

20000 20000 7500

23084170

30000

2400 2400 7300 NOTE 1’ BIS 20000 20000 2400 7300 NOTE 1’ BIS 30000

23069115 23069591

30000 NOTE 1 30000 NOTE 1 20000 NOTE2 8400 30000

30000 NOTE 1 30000 NOTE 1 20000 NOTE 2 8400 30000

23070664 23079946

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components

DESCRIPTION

ST Nº

HP turbine wheels continued HP turbine wheels

1st

23088784

2nd

23069438

P/N

23074462 23074644 23075345

1st-to 2nd turbine spacer

3rd

LP turbine wheels

1st

23084520 23084781 23070989 23072849 23075364 23076778 23060111 23070355 23073957

2nd

23074586 23074587 23076801 23058312 23070356 23074270 23074308 23074312 23079220 23079221

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 8-1-11

Rolls-Royce AE3007 Engine Model-Life Limit (FC) A1 A1P 30000 30000 10000 20000 NOTE 3 20000 20000 30000 20000 NOTE 4 23000 20000 13100 13100 13100 30000 30000 NOTE 5 20000 NOTE 6 30000 NOTE 5 30000 NOTE 5 20000 NOTE 6 30000 30000 30000 30000 NOTE 5 20000 NOTE 7 30000 NOTE 5 30000 30000 30000 30000 30000

10000 20000 NOTE 3 20000 20000 30000 20000 NOTE 4 23000 20000 12900 12900 12900 30000 30000 NOTE 5 20000 NOTE 6 30000 NOTE 5 30000 NOTE 5 20000 NOTE 6 30000 30000 30000 30000 NOTE 5 20000 NOTE 7 30000 NOTE 5 30000 30000 30000 30000 30000

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components

DESCRIPTION

ST Nº

LP turbine wheels continued

3rd

23070046

LP Turbine interstage spacer

4th

23070357 23079224 23054049

LP Turbine forward shaft

5th

P/N

23059694 23067076 23074538 23078229

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 8-1-12

Rolls-Royce AE3007 Engine Model-Life Limit (FC) A1 A1P 30000 NOTE 5 30000 NOTE 5 20000 NOTE 8 20000 NOTE 8 30000 NOTE 5 30000 NOTE 5 30000 30000 30000 NOTE 5 30000 NOTE 5

24000 30000 30000 30000

20000 30000 30000 30000

NOTE: (1) The total in-service history for a life limited part must be reviewed prior to installation. If the engine was upgraded from an AE3007A to an AE 3007A1 or AE 3007 A1P engine you will have to find the cycle life limit. See table 1 NOTE: (1’ bis) Accumulated life limit only for cone assemblies processed with the slurry deburr. See table 1’ bis NOTE: (2) Certain HP turbine Stage 1 wheel serial numbers remain at the 20,000 cycle life limit. See Table 2 NOTE: (3) Accumulated Cycle life limit only for wheels in engines that have complied Service Bulletin AE 3007A-72-176 or Service bulletin AE 3007A-72-215, or both NOTE: (4) Certain HP turbine Stage 2 Wheel serial numbers remain at the 20,000 cycle life limit. See table 3 NOTE: (5) The total in-service history for a life limited part must be reviewed prior to installation. If the engine was upgraded from an AE3007A to an AE 3007A1 or AE 3007 A1P engine you will have to find the cycle life limit. See table 1 NOTE: (6) Certain LP turbine Stage 1 wheel serial numbers remain at the 20, 000 cycle life limit. See table 5

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 8-1-13

NOTE: (7) Certain LP turbine Stage 2 wheel serial numbers remain at the 20, 000 cycle life limit. See table 6 NOTE: (8) certain LP turbine Stage 3 wheel serial numbers remain at the 20, 000 cycle life limit. See table 7 TABLE 1 – AE 3007A1 CHAPTER 5 CYCLE LIFE LIMIT AFTER CONVERSION FROM AE3007A

ENGEIN CYLCES ACCUMULATED AS AE3007A

NEW CHAPTER AFTER CYLCE LIFE LIMIT

1 - 1000 1001 – 2000 2001 - 3000 3001 - 4000 4001 - 5000 5001 - 6000 6001 - 7000 7001 - 8000 8001 - 9000 9001 - 10000 10000 - 11000 11001 - 12000 12001 - 13000 13001 - 14000 14001 +

29500 29000 28500 28000 27500 27000 26500 26000 25500 25000 24500 24000 23500 23000 20000

TABLE 1’ BIS – COMPRESOR SHAFT CONE ASSEMBLIES PROCESSED WITH SLURRY DEBURR

MM78599 MM78615

P/N 23070729 or 23076017**(BY ENGINE AE3007A1P AFFECTED SERIAL NUMBERS MM78652 MM78660 MM78653 MM78661 MM78654 MM78662 MM78655 MM78663

F-GAC-01 SEP-07

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components MM78632

MM78656 MM78657 MM78658 MM78659

MM78650 MM78651

Page: 8-1-14

-MM78665 and up

(**) The double asterisk indicates the serial number may be associated with either part number. TABLE 2 – HP Turbine Stage 1 Wheel Serial

MM119837 MM142683 MM142812 MM142819 MM142827 MM142843 MM142870 MM142873 MM142944 MM142956 MM142969 MM142977 MM142991 MM142993 MM143087

P/N 23069591 (BY ENGINE AE3007A AND AE3007A1P AFFECTED SERIAL NUMBERS MM143107 MM500591 MM143255 MM500647 MM143272 MM500665 MM143309 MM500685 MM182400 MM500724 MM182632 MM500807 MM182653 MM500835 MM182691 MM500890 MM182734 MM500924 MM182761 MM500937 MM182803 MM500944 MM182811 MM500948 MM182842 MM500950 MM183020 MM500955 MM500563 MM500957

MM500958 MM500962 MM504103 MM504105 MM504108 MM504155 MM504182 MM504185 MM504194 MM504230 MM504444 MM504589 MM507799

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 8-1-15

TABLE 3 – HP Turbine Stage 2 Wheel Serial Numbers Remaining at a 20, 00 Cycle Life Limit

MM504926

P/N 23075345 (BY ENGINE AE3007A AND AE3007A1P) AFFECTED SERIAL NUMBERS MM508446

TABLE 4 - AE 3007A1 CHAPTER 5 CYCLE LIFE LIMIT AFTER CONVERSION FROM AE3007A

ENGEIN CYLCES ACCUMULATED AS AE3007A

NEW CHAPTER AFTER CYLCE LIFE LIMIT

1 - 1000 1001 – 2000 2001 - 3000 3001 - 4000 4001 - 5000 5001 - 6000 6001 - 7000 7001 - 8000 8001 - 9000 9001 - 10000 10000 - 11000 11001 - 12000 12001 - 13000 13001 - 14000 14001 +

29500 29000 28500 28000 27500 27000 26500 26000 25500 25000 24500 24000 23500 23000 20000

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 8-1-16

TABLE 5 – LP Turbine Stage 1 Wheel Serial Numbers Remaining at a 20, 000 Cycle Life Limit

(BY ENGINE AE3007A AND AE3007A1P P/N 23060111 AFFECTED SERIAL NUMBERS GX51818 GX51820 WD53865 WD53867 WD53867 WD53874 WD62757 WD62761

WD76521 WD89206 WD131885 WD209960 WY13069 WY13102 WY45724 WY45735

WY45737 WY45739 WY45744 WY45746 WY45747 WY45749 WY45758 WY46589

WY46592 WY46594 WY46596 WY46827 WY46833

P/N 23073957 AFFECTED SERIAL NUMBERS WD245173

TABLE 5 – LP Turbine Stage 2 Wheel Serial numbers remaining at a 20, 000 cycle life limit P/N 23058312 (BY ENGINE AE3007A AND AE3007A1P AFFECTED SERIAL NUMBERS WD76723 WY46843 WY45630 WY46859 WY45652

WD212941 WD212953 WD53644

TABLE 6 – LP Turbine Stage # Wheel Serial numbers remaining at a 20, 00 Cycle limit

WD188051

WD80520

P/N 23070046 (BY ENGINE AE3007A AND AE3007A1P AFFECTED SERIAL NUMBERS WD80563 WY13880

WY13924

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145 EMB 145 Maintenance Program SECCIÓN 8. COMPONENTES LIMITADOS POR VIDA Life Limit Components

Código: M-PME-01 Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 8-1-17

CHAPTER 78 THRUST REVERSER DESCRIPTION Primary Door Lock Actuator Primary Door Lock Actuator Pivot Door Actuator Pivot Door Actuator Pivot Door Actuator Pivot Door Actuator Pivot Door Actuator Pivot Door Actuator Pivot Door Actuator Pivot Door Actuator Pivot Door Actuator Pivot Door Actuator Directional Control Unit Lock Sequencer Lock Sequencer Lock Sequencer Tertiary lock Tertiary lock Tertiary lock Tertiary lock Isolation Control Unit Isolation Control Unit Isolation Control Unit Isolation Control Unit

PART NUMBER TY2038-01A TY2038-02A TY2039-03A TY2039-03B TY2039-03C TY2039-05B TY2039-05B-629 TY2039-05B629TY2039-05B-7 TY2039-10A TY2039-11A TY2039-14A TY2040-01A TY2047-02A TY2047-03A TY2047-03B TY2037-02A TY2138-01A TY2138-01B TY2560-01A TY2041-03A TY2041-02B TY2041-02A TY2041-01A

SUPPLIER LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS LUCAS

LIFE LIMIT (*) 60,250 TRC 60,250 TRC 1,800 TRC 1,800 TRC 1,800 TRC 15,000 TRC 15,000 TRC 60,250 TRC 60,250 TRC 15,000 TRC 60,250 TRC 60,250 TRC 60,250 TRC 60,250 TRC 60,250 TRC 60,250 TRC 1,500 TRC 13,100 TRC 13,100 TRC 61,500 TRC 60,250 TRC 1,932 TRC 1,932 TRC 1,932 TRC

EFECTIVITY ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL

* NOTE: Every time the Trust Reverser is operated must be considered one Thrust Reverser Cycle (TRC), either in normal operation or power Back operation in the authorized aircraft.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 9. REQUERIMIENTOS DE MANTENIMIENTO CATEGORIA II

Fecha de Efectividad: 05-Abr-10 Page: 9 -1- 1 .

"CATEGORY II MAINTENANCE REQUIEREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

22-11-00-720-003-A00

SYSTEMS

FNC

CAT II

Functionally Check Category II monitoring function

30-41-00-710-001-A00

SYSTEMS

OPC

CAT II

30-42-00-710-001-A00

34-01-00-720-001-A00

SYSTEMS

SYSTEMS

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

Maintenance Program Requirement for Cat. II Operation (Applicable until Aerolitoral Cat.II operation is certified)

A8

800 FH

ALL

Operationally Check Windshield Wiper

Maintenance Program Requirement for Cat. II Operation (Applicable until Aerolitoral Cat.II operation is certified)

A8

C

ALL

OPC

CAT II

Operationally Check Windshield Heating

Recommended Task prior to the Winter (October) in stead of "C CHECK" and Maint. Program requirement for Cat. II Operation

3

C

ALL

FNC

Or according to Local Authorities requirements. ISIS configurated aircraft only and Maintenance Program CAT Functionally Check Integrated Standby Instrument System - ISIS Requirement for Cat. II Operation II (Applicable until Aerolitoral Cat.II operation is certified)

3

C

ALL

Functionally Check Standby Altimeter Indicator

Or according to Local Authorities requirements. Maintenance Program Requirement for Cat. II Operation (Applicable until Aerolitoral Cat.II operation is certified)

3

C

ALL

Descripción / Description

34-11-00-720-001-A00

SYSTEMS

FNC

CAT II

34-12-00-720-001-A00

SYSTEMS

FNC

CAT II

Functionally Check Standby Airspeed Indicator

Maintenance Program Requirement for Cat. II Operation (Applicable until Aerolitoral Cat.II operation is certified)

A8

C

ALL

34-13-00-790-001-A00

SYSTEMS

FNC

CAT II

Functionally Check Pitot-Static System for Leakage

Maintenance Program Requirement for Cat. II Operation (Applicable until Aerolitoral Cat.II operation is certified)

3

C

ALL

3

C

ALL

34-15-00-720-001-A00

SYSTEMS

FNC

CAT II

Functionally Check ADC system

Or 24 MOS, whichever occurs first. Maintenance Program Requirement for Cat. II Operation (Applicable until Aerolitoral Cat.II operation is certified) NOTE: Interval in accordance with MRB section 3

34-24-00-710-001-A00

SYSTEMS

OPC

CAT II

Operationally Check Standby Attitude Indicator.

Maintenance Program Requirement for Cat. II Operation (Applicable until Aerolitoral Cat.II operation is certified)

A8

C

ALL

34-41-00-710-001-A00

SYSTEMS

OPC

CAT II

Operationally Check GPWS/Windshear

Maintenance Program Requirement for Cat. II Operation

-

C

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 9. REQUERIMIENTOS DE MANTENIMIENTO CATEGORIA II

Fecha de Efectividad: 05-Abr-10 Page: 9 -1- 2 .

"CATEGORY II MAINTENANCE REQUIEREMENTS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

34-41-00-710-003-A00

SYSTEMS

OPC

CAT II

Descripción / Description

Operationally Check EGPWS / Windshear

Maintenance Program Requirement for Cat. II Operation (Applicable until Aerolitoral Cat.II operation is certified)

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

3

C

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 1

SECCIÓN 10. REDUCCION DEL LIMITE SE SEPARACION VERTICAL

Fecha de Efectividad: 20-Sep-09 Page: 10 -1- 1 .

"REDUCE VERTICAL SEPARATION MINIMUM (RVSM)" Número de Tarea Task Number

Grupo Group

Tipo Type

22-11-00-720-004-A00

SYSTEMS

FNC

34-13-04-280-001-A00

SYSTEMS

SDI

RVS M

Inspect (Special Inspection) RVSM Critical Region (Skin) for Waviness. (aircraft identified in and have not accomplished SB 145-34-0110).

34-13-04-280-001-A01

SYSTEMS

SDI

6

Inspect (Special Inspection) RVSM Critical Region (Skin) for Waviness (including aircraft identified in and are Post-Mod SB 145-34-0110).

34-13-04-280-002-A00

SYSTEMS

SDI

RVS M

Inspect (Special Inspection) Static Port Surrounding Plate for Flushness and Integrity. Flushness and Integrity (aircraft identified in And have not accomplished SB 145-34-0110)

34-13-04-280-002-A01

SYSTEMS

SDI

6

Inspect (Special Inspection) Static Port Surrounding Plate for Flushness and Integrity (including aircraft identified in and are Post-Mod SB 145-34-0110).

34-13-04-280-003-A00

34-13-04-280-003-A01

SYSTEMS

SYSTEMS

Cat. Cat. RVS M

Intervalo Interval

Efectividad Effect.

4000 FH

ALL

-

24 MOS

ALL

-

C

ALL

-

24 MOS

ALL

-

C

ALL

SDI

Inspect (Special Inspection) Passenger Gaseous Oxygen Service Panel (panel P/N 145-51705-001, attached by livelock RVS stud xnut) installed in RVSM critical region for Flushness and M Integrity (aircraft identified in and have not accomplished SB 14534-0110).

-

24MOS

ALL

SDI

Inspect (Special Inspection) Passenger Gaseous Oxygen Service Panel (panel P/N 145-51705-001, attached by livelock stud xnut) installed in RVSM critical region for Flushness and Integrity (including aircraft identified in and are Post-Mod SB 14534-0110).

-

C

ALL

6

Descripción / Description

Umbral Thrsld.

Functionally Check AFCS Altitude Hold Mode and Altitude PreSelect Mode. Maintenance Program Requirement for RVSM Operation

Maintenance Program Requirement for RVSM Operation

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 11. LIMITACIONES DEL SISTEMA DE COMBUSTIBLE

Fecha de Efectividad: 05-Abr-10 Page: 11 -1-1 .

"FUEL SYSTEM LIMITATIONS" Número de Tarea Task Number

Grupo Group

Tipo Type

28-11-00-720-001-A00

SYSTEMS

Cat. Cat.

Descripción / Description

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

FNC

Functionally Check critical bonding integrity of selected conduits Comply BAD 2007-08-02 AND AD 2008inside the wing tank, Fuel pump and FQIS connectors at tank 13-14 wall by conductivity measurements.

-

30000 FH

ALL

Applicable to all Aerolitoral ERJ145 fleet Comply BAD 2000-08-01R3 and AD 2005-13-22 Comply BAD 2007-08-02 AND AD 2008-13-14

-

8000 FH

ALL

-

20000 FH

ALL

-

20000 FH

ALL

-

10000 FH

ALL

-

20000 FH

ALL

28-21-01-220-001-A00

SYSTEMS

DET

AD

Inspect Electric Fuel Pump Connector

28-23-03-220-001-A00

SYSTEMS

DET

Inspect Pilot Valve Harness inside the conduit

28-23-04-220-001-A00

SYSTEMS

DET

Inspect Vent Valve Harness inside the conduit

28-41-01-720-001-A00

SYSTEMS

FNC

Functionally Check Fuel Conditioning (FCU)

28-41-03-220-001-A00

SYSTEMS

DET

Inspect FQIS harness for clamp and wire jacket integrity

Comply BAD 2007-08-02 AND AD 200813-14 Comply BAD 2007-08-02 AND AD 200813-14 Comply BAD 2007-08-02 AND AD 200813-14 Comply BAD 2007-08-02 AND AD 200813-14

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 12. TAREAS RECOMENDADAS

Fecha de Efectividad: 05-Abr-10 Page: 12 -1- 1 .

"RECOMENDED MAINTENANCE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval 100 FH / 14 DY

Efectividad Effect.

12-15-01-610-001-A00

SYSTEMS

SVC

REC

Toilet Water Servicing

-

12-15-02-610-001-A00

SYSTEMS

SVC

REC

Sterilize Water Reservoir

-

C

ALL

21-23-05-710-001-A00

SYSTEMS

OPC

-

5A (*)

ALL

21-25-01-211-001-A00

SYSTEMS

VCK

REC

21-51-02-170-002-A00

SYSTEMS

RST

REC

Visually Check Ram Air Flap Valve

-

2A

ALL

Clean Dual Heat Exchanger on the Aircraft.

-

3A

21-51-13-211-001-A00

SYSTEMS

VCK

REC

Visually Check Water Spray Nozzles

ALL

-

A

ALL

-

C

ALL

Descripción / Description

Operationally Check Toilet Gasper Hose Filter (if installed).

Replace Torque Motor Dual Valve Air Filter Element

(*)Initial inspection since new, "C" check.

Only to aircraft Post-Mod SB 145-210039. TMDV P/N: C143123-4 ONLY

ALL

21-60-08-960-001-A00

SYSTEMS

DIS

REC

23-12-04-212-001-A00

SYSTEMS

GVI

REC

Visual Inspection of the VHF Antenna for cracks

-

C

ALL

-

C

ALL ALL

23-31-00-710-002-A00

SYSTEMS

OPC

REC

Operationally Check Back-up/Emergency Cabin Interphone System

23-31-00-710-003-A00

SYSTEMS

OPC

REC

Operationally Check Loudspeakers

-

C

23-51-00-710-002-A00

SYSTEMS

OPC

REC

Audio System Operational Test.

-

C

ALL

24-34-01-900-002-A00

SYSTEMS

RST

REC

Restore APU Starter Generator

-

800 AH

ALL

25-11-01-140-001-A00

SYSTEMS

SVC

REC

Cleaning and Lubrication of Locking Pins of the Pilot and Copilot Seats

-

A

ALL

-

A

ALL

DET

Inspect (Detailed Inspection) Lavatory Waste Disposal Door

Inspect and correct all defects found on all lavatory paper and linen waste receptacle enclosure access doors and disposal doors for proper operation, fit, sealing, and latching for the containment of possible trash fires. COMPLY AD 7408-09 R2 paragraph e)1 & e)2

REC

Check Hydraulic Fluid (Analysis)

Send to Laboratory for Analysis

-

C

ALL

REC

Functionally Check Rain Repellent Coating (RRC)

If installed

-

A

ALL

Inspect (Visual Inspection) the Main Landing Gear Doors Polyurethane Film for integrity. NOTE: Zones 722 and 732.

-

5A

ALL

Inspect (Visual Inspection) the Nose Landing Gear Doors Polyurethane Film for integrity. NOTE: Zones 713 and 714.

-

5A

ALL

25-40-01-220-001-A00

SYSTEMS

AD

29-10-00-280-001-A00

SYSTEMS

SDI

30-44-04-720-001-A00

SYSTEMS

FNC

32-10-07-212-001-A00

SYSTEMS

GVI

REC

32-20-07-212-001-A00

SYSTEMS

GVI

REC

33-11-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Cockpit Lights

-

C

ALL

33-12-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Instrument and Control Panel Lighting

-

C

ALL

33-15-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Flood/Storm Lights

-

C

ALL

33-21-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Passenger Cabin Lights

-

C

ALL

33-23-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Passenger Warning Signs

-

C

ALL

33-25-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Reading and Attendant Call Lights

-

C

ALL

33-26-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Courtesy/Stair Lights

-

C

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 12. TAREAS RECOMENDADAS

Fecha de Efectividad: 05-Abr-10 Page: 12 -1- 2 .

"RECOMENDED MAINTENANCE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

33-28-00-710-001-A00

SYSTEMS

OPC

REC

33-29-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Lavatory Lights

-

C

ALL

Operationally Test Galley Lights

-

C

33-30-00-710-001-A00

SYSTEMS

OPC

ALL

REC

Operationally Test Baggage and Service Compartments

-

C

ALL

33-41-00-710-001-A00

SYSTEMS

33-42-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Landing Lights

-

C

ALL

OPC

REC

Operationally Test Taxi Lights

-

C

33-43-00-710-001-A00

ALL

SYSTEMS

OPC

REC

Operationally Test Navigation Lights

-

C

ALL

33-44-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Inspection Lights

-

C

ALL

33-46-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Logotype Lights

-

C

ALL

33-47-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Anti-collision Lights

-

C

ALL

35-10-00-910-001-A00

SYSTEMS

FNC

REC

Leak Test Crew Oxygen System Lines

-

36 MOS

ALL

38-30-00-610-001-A00

SYSTEMS

SVC

REC

Toilet Waste Bowl Servicing

-

45-45-00-970-001-A00

SYSTEMS

DRC

REC

CMC DATA - MFD Downloading

-

52-14-01-220-001-A00

SYSTEMS

DVI

REC

52-31-00-710-001-A00

SYSTEMS

OPC

REC

53-04-02-212-001-A00

SYSTEMS

GVI

REC

53-11-01-220-001-A00

SYSTEMS

DVI

53-11-05-212-001-A00

SYSTEMS

Descripción / Description

Together with Task 35-10-07-720-001A00 and 35-10-07-720-002-A00

Inspect (Detailed Inspection) Main Door Drain Valves for Obstruction or Damage Operational Check Baggage Door Actuating and Locking Mechanism

100 FH / 14 DY 100 FH / 14 DY

ALL ALL

-

C

ALL

-

5A

ALL

Inspect (Visual Inspection) the Naca-Air-Intake at Forward WingTo- Fuselage Fairing Polyurethane Film for Integrity. NOTE: Zone 191.

-

5A

ALL

REC

Inspect (Detailed Inspection) the Presence of Water on the Radome

-

C

ALL

GVI

REC

Inspect (Visual Inspection) the Radome Polyurethane Film

-

A

ALL

-

5A

ALL

53-11-06-212-001-A00

SYSTEMS

GVI

Inspect (Visual Inspection) the Naca-Air-Intake at Forward WingTo- Fuselage Fairing Polyurethane Film for Integrity. NOTE: REC Zones 113 and 114.

55-10-00-212-001-A00

SYSTEMS

GVI

REC

Inspect (Visual Inspection) the Horizontal Stabilizer LeadingEdge Root-Fairing and Horizontal Stabilizer-Tip Polyurethane Film for Integrity. NOTE: Zones 333 and 334.

-

5A

ALL

55-30-00-212-001-A00

SYSTEMS

GVI

REC

Inspect (Visual Inspection) the Vertical Stabilizer Leading-Edge Polyurethane Film for integrity. NOTE: Zone 323.

-

5A

ALL

56-10-01-720-001-A00

SYSTEMS

FNC

REC

Functionally Check Torque of Windshield Attaching Bolts

Pre SB 145-56-0006

-

5A

ALL

56-10-01-720-001-A01

SYSTEMS

FNC

REC

Functionally Check Torque of Windshield Attaching Bolts

Post SB 145-56-0006.

-

2C

ALL

56-10-01-720-002-A00

SYSTEMS

FNC

REC Functionally Check Windshield Anti-Static Coating for Continuity

-

2C

ALL

56-20-01-220-001-A00

SYSTEMS

DVI

REC

-

C

ALL

Inspect (Detailed Inspection) Passenger Cabin Windows for Delamination

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2

SECCIÓN 12. TAREAS RECOMENDADAS

Fecha de Efectividad: 05-Abr-10 Page: 12 -1- 3 .

"RECOMENDED MAINTENANCE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

57-43-00-212-001-A00

SYSTEMS

GVI

REC

76-12-01-212-001-A00

SYSTEMS

GVI

REC

Descripción / Description Inspection (Visual Inspect) the Wing-Tip Polyurethane Film for Integrity. NOTE: Zones 561 and 661. Inspect (Visual Inspection) Resolve Attachments to the Thrust Levers

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

5A

ALL

-

2C

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 13 -1- 1 .

SECCIÓN 13.TAREAS DE COMPONENTES REEMPLAZO MANTENIMIENTO LINEA "COMPONENT TASKS REPLACES BY LINE MAINTENANCE" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

21-51-02-170-001-A00

SYSTEMS

RST

6

Descripción / Description Clean Dual Heat Exchanger and Visually Check condition of core Only to aircraft Post-Mod SB 145-21-0039. TMDV P/N: C143123-4 ONLY (Not applicable 795,798,803,852, 861)

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

C

ALL

-

C

ALL

-

24 MOS

ALL

-

72 MOS

ALL ALL

21-60-08-960-001-A00

SYSTEMS

DIS

REC

Replace Torque Motor Dual Valve Air Filter Element

23-71-02-710-001-A00

SYSTEMS

OPC

9

Operationally Check CVR Underwater Locator Beacon

23-71-02-960-001-A00

SYSTEMS

DIS

9

Discard CVR Underwater Locator Beacon Battery

24-31-01-900-001-A01

SYSTEMS

RST

7

Restore Main Generator

-

4000 FH

24-34-01-900-002-A00

SYSTEMS

RST

REC

Restore APU Starter Generator

-

800 AH

ALL

24-34-01-960-001-A00

SYSTEMS

DIS

7

Discard APU Starter/Generator Brushes

-

800 AH

ALL

24-35-01-900-001-A00

SYSTEMS

RST

8

Restore Back-up Battery

-

12 MOS

ALL

24-36-01-610-001-A00

SYSTEMS

SVC

6

24-36-01-610-001-A02

SYSTEMS

SVC

6

24-36-01-720-001-A00

SYSTEMS

FNC

24-36-01-900-001-A00

SYSTEMS

RST

25-61-00-212-001-A00

SYSTEMS

GVI

8

25-61-00-710-001-A00

SYSTEMS

OPC

8

Operationally Check Emergency Locator Transmitter System- Proper Operation- Crash Switch Operation

25-61-04-960-001-A00

SYSTEMS

DIS

8

Replace ELT battery ARTEX P/N: 452-0130

25-61-04-960-001-A01

SYSTEMS

DIS

8

Replace ELT battery SOCATA P/N: ELT90A2560102000

25-61-04-960-001-A02

SYSTEMS

DIS

8

Replace ELT battery ARTEX P/N 452-0133 and L94

26-15-00-720-001-A00

SYSTEMS

FNC

8

26-15-01-212-001-A00

SYSTEMS

VCK

8

26-15-01-960-001-A00

SYSTEMS

DIS

8

Discard JAMCO Baggage Compartment Smoke Detector

ULB battery change in accordance with manufacturer's dataplate expiration date Applicable to P/N: 30086-011 ONLY

Service Main Battery

Interval according to manufacturer's recommendation. MARATHON N/P: 32248-001 ONLY

-

500 FH

ALL

Service Main Battery

MARATHON M3 N/P: 32845-001 ONLY

-

2000 FH

ALL

6

Functionally Check Main Battery

SAFT N/P: 442CH1 ONLY

-

1000 FH

ALL

8

Restore Main Battery Inspect (General Visual) Emergency Locator Transmitter for Condition, Expiration Date of Battery, Proper Installation, Battery Corrosion and Leakage

SAFT N/P: 442CH1 ONLY Or according to Local Authorities' requirements.Follow manufacturer's recommendation. Or according to Local Authorities' requirements. Follow manufacturer's recommendation. (*) ELT Battery change in accordance with manufactuirer data plate expiration date or Local Regulatory Authority Requirements . (*) ELT Battery change in accordance with manufactuirer data plate expiration date or Local Regulatory Authority Requirements ELT battery change in accordance with manufacturer data plate expiration date or Local Regulatory Authority Requirements.

-

12 MOS

ALL

-

12 MOS

ALL

-

12 MOS

ALL

-

26 MOS

ALL

-

48 MOS

ALL

-

60 MO

ALL

-

A / 3 MOS

ALL

-

4A

ALL

-

180 MOS

ALL

-

12 MOS

ALL

-

60 MOS

ALL

-

60 MOS

ALL

-

72 MOS

ALL

-

12 MOS

ALL

Functionally Check JAMCO Baggage Compartment Smoke Detection System (actuating each smoke sensor in the baggage compartment with a smoke tester) Visually Check WALTER KIDDE Baggage Compartment Smoke Detection System Maintenance LED

26-21-02-280-001-A00

SYSTEMS

SDI

9

Inspect Engine Fire Extinguishing Bottle for Weight and Check Bottle Pressure

26-21-02-720-001-A00

SYSTEMS

FNC

9

Perform Hydrostatic Check of the Engine Fire Extinguishing Bottle

26-21-03-720-001-A00

SYSTEMS

FNC

9

Functionally Check Engine Fire Extinguishing Bottle Pressure Switch

26-21-04-960-001-A00

SYSTEMS

DIS

9

Discard Engine Fire Extinguishing Bottle Cartridges

26-22-01-280-001-A00

SYSTEMS

SDI

9

Inspect APU Fire Extinguishing Bottle for Weight and Check Bottle Pressure

Or according to Local Authorities Requirements.

As per the manufacturer's recommendation, Check at each bottle Hydrostatic Test (60MOS). 108 months from date of manufacture or 72 months from date of installation whichever occurs first Or according to Local Authorities Requirements.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 13 -1- 2 .

SECCIÓN 13.TAREAS DE COMPONENTES REEMPLAZO MANTENIMIENTO LINEA "COMPONENT TASKS REPLACES BY LINE MAINTENANCE" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

26-22-01-720-001-A00

SYSTEMS

FNC

9

Descripción / Description Perform Hydrostatic Check of APU Fire Extinguishing Bottle As per the manufacturer's recommendation, Functionally Check APU Fire Extinguishing Bottle Pressure Switch Check at each bottle Hydrostatic Test (60MOS). 108 months from date of manufacture or 72 Discard APU Fire Extinguishing Bottle Cartridges months from date of installation whichever occurs first Class "C" Baggage Compartment only Perform Inspect Baggage Compartment Fire Extinguishing Bottles (high rate and an Hydrostatic Test at each 60 MOS metering) for weight. (Applicable All Aerolitoral ERJ-145 Fleet) Perform Hydrostastic Check of Baggage Fire Extinguishing Bottles (HIGH RATE & METERING) Class "C" Baggage compartment only 180 Discard Baggage Fire Extinguishing Bottles (high rate and metering) months from date of manufacture (DOM) or Cartridges 120 from date of installation, whichever ocurs first. (applicable All Aerolitoral ERJ-145 Fleet) Or according to Local Authorities Inspect Portable Fire Extinguishing Bottle for Weight (See placard Requirements. Interval follows manufacturer's attached to the bottle.) recommendation. (WETTING Agent Only) Or in accordance with Perform Hydrostatic Check of portable Fire Extinguishing Bottles Local Regulatory Authority Requirements (Not (WETTING Agent Only) P/N 892480 applicable All Aerolitoral ERJ145 fleet) (HALON Agent Only) Or in accordance with Perform Hydrostatic Check of portable Fire Extinguishing Bottles (HALON Local Regulatory Authority Requirements Agent Only) P/N 100-9750, 466090, 898052, A352 Series and C352 (Applicable All Aerolitoral ERJ-145 Fleet) Inspect Lavatory Fire Extinguisher Bottle for Weight

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

60 MOS

ALL

-

60 MOS

ALL

-

72 MOS

ALL

-

12 MOS

ALL

-

60 MOS

ALL

-

120 MOS

ALL

-

12 MOS

ALL

-

60 MOS

ALL

-

144 MOS

ALL

12 MO

ALL

-

10000 FH

ALL

26-22-02-720-001-A00

SYSTEMS

FNC

9

26-22-03-960-001-A00

SYSTEMS

DIS

9

26-23-01-280-001-A00

SYSTEMS

SDI

6

26-23-01-720-001-A00

SYSTEMS

FNC

6

26-23-02-960-001-A00

SYSTEMS

DIS

6

26-24-00-280-001-A00

SYSTEMS

SDI

9

26-24-01-720-001-A00

SYSTEMS

FNC

8

26-24-01-720-001-A01

SYSTEMS

FNC

8

26-25-01-280-001-A00

SYSTEMS

SDI

6

28-41-01-720-001-A00

SYSTEMS

FNC

29-10-04-900-001-A00

SYSTEMS

DIS

7

Replace EMDP Brushes

-

6000 FH

ALL

31-31-00-710-001-A00

SYSTEMS

DRC

9

FDR Data-Personal computer Downloading

-

12 MOS

ALL

31-31-02-710-001-A00

SYSTEMS

OPC

9

Operationally Check FDR Underwater Locator Beacon

-

24 MOS

ALL

31-31-02-960-001-A00

SYSTEMS

DIS

9

Discard FDR Underwater Locator Beacon Battery

-

72 MOS

ALL

-

5000 FC

ALL

-

5A / 15 MOS

ALL

-

5000 FC

ALL

32-10-00-210-801-A00

Functionally Check Fuel Conditioning (FCU)

Externally inspect the MAIN LANDING GEAR components: • Trailing arm MLG (SSI 32-10-03) Service MLG Shock Absorber Externally inspect the NOSE LANDING GEAR components: • Strut (main fitting) - NLG (SSI 32-20-12)

Comply BAD 2007-08-02 AND AD 2008-13-14

ULB Battery Change in accordance with manufacturer data plate expiration date

STRUCTURAL

GVI

-

32-10-02-610-001-A00

SYSTEMS

SVC

9

32-20-00-210-801-A00

STRUCTURAL

GVI

-

32-20-00-210-802-A00

STRUCTURAL

GVI

-

Externally inspect the NOSE LANDING GEAR components: • Auxiliary Drag Strut Bottom stay (SSI 32-20-16)

-

5000 FC

ALL

32-20-00-210-803-A00

STRUCTURAL

GVI

-

Externally inspect the NOSE LANDING GEAR components: • Main Drag Strut Top stay - NLG (SSI 32-20-13)

-

5000 FC

ALL

32-20-00-210-804-A00

STRUCTURAL

GVI

-

Externally inspect the NOSE LANDING GEAR components: • Auxiliary Drag Strut Top stay (SSI 32-20-15)

-

5000 FC

ALL

32-20-01-610-001-A00

SYSTEMS

SVC

9

Service NLG Shock Absorber

-

5A / 15 MOS

ALL

32-20-01-720-001-A00

SYSTEMS

FNC

8

Functionally Check NLG Leg for Centering Cam Play

-

144 MOS

ALL

5A Or 15 MOS, whichever occurs first.

5A Or 15 MOS, whichever occurs first. 20000 FC Or 144 MOS, whichever occurs first. Perform the check at the time of NLG Restoration.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 13 -1- 3 .

SECCIÓN 13.TAREAS DE COMPONENTES REEMPLAZO MANTENIMIENTO LINEA "COMPONENT TASKS REPLACES BY LINE MAINTENANCE" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Descripción / Description

34-11-00-720-001-A00

SYSTEMS

FNC

CAT II

Functionally Check Standby Altimeter Indicator

34-25-00-720-001-A00

SYSTEMS

FNC

6

Functionally Check Standby Compass for proper compensation

34-52-00-720-001-A00

SYSTEMS

FNC

6

Functionally Check Transponder System

35-10-00-910-001-A00

SYSTEMS

FNC

REC

Leak Test Crew Oxygen System Lines

8

Functionally Check Crew Oxygen Cylinder Pressure Regulator NOTE: At the time of Cyl. Hydrostatic Test.

35-10-07-720-001-A00

SYSTEMS

FNC

Or according to Local Authorities requirements. Maintenance Program Requirement for Cat. II Operation (Applicable until Aerolitoral Cat.II operation is certified) Or according to Local Authorities requirements. Or according to Local Authorities Together with Task 35-10-07-720-001-A00 and 35-10-07-720-002-A00 At the time of Cylinder Hydrostatic Test. Or according to Local Authorities requirements. Aircraft Equipped with Chemical Oxygen System Only.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

3

C

ALL

-

24 MOS

ALL

-

24 MOS

ALL

-

36 MOS

ALL

-

36 MOS

ALL

-

36 MOS

ALL

-

180 MOS

ALL

35-10-07-720-002-A00

SYSTEMS

FNC

9

Functionally Check (Hydrostatic Test) Crew Oxygen Cylinder

35-20-01-960-001-A00

SYSTEMS

DIS

8

Replace/Discard Chemical Oxygen Generator

35-30-01-720-001-A00

SYSTEMS

FNC

9

Functionally Check Portable Oxygen Cylinder Pressure Regulator NOTE: At the time of Cylinder Hydrostatic Test.

At the time of Cylinder Hydrostatic Test.

-

60 MOS

ALL

35-30-01-720-002-A00

SYSTEMS

FNC

9

Functionally Check (Hydrostatic Test) Portable Oxygen Cylinder

Or according to Local Authorities' requirements.

-

60 MOS

ALL

35-30-03-960-001-A00

SYSTEMS

DIS

8

36-10-01-130-001-A00

SYSTEMS

RST

6

36-11-01-220-001-A00

SYSTEMS

DVI

6

36-11-02-130-001-A00

SYSTEMS

RST

9

Discard Protective Breathing Equipment PN MR10042N, 15-40F-11,1540F-10, 15-40F and E28180-10 Clean Crossbleed Valve Filter by Ultrasonic Method Inspect (Detailed Inspection) Engine Low Pressure Bleed Air Check Valve. P/N 816603-3 Clean High-Stage Valve Filter by Ultrasonic Method

36-11-03-130-001-A00

SYSTEMS

RST

6

Clean Fan Air Valve Filter by Ultrasonic Method

36-11-04-110-001-A00

SYSTEMS

RST

6

Clean Pre-Cooler by Chemical Method

36-11-05-130-001-A00

SYSTEMS

RST

6

Clean Engine Bleed Valve Filter by Ultrasonic Method

49-17-00-160-001-A00

SYSTEMS

RST

9

Clean APU Drains Post-Mod SB 145-49-0029

-

120 MOS

ALL

-

C

ALL

-

C

ALL

-

C

ALL

-

C

ALL

-

6000 FH

ALL

-

C

ALL

-

C

ALL

-

400 AH

ALL

-

800 AH

ALL

-

1200 AH

ALL

According to Manufacturer's recommendation.

-

1200 AH

ALL

Check Oil Level and Service Oil System as required Ref a 49-96-00-200According to manufacturer's recommendation. 801-A

-

400 AH

ALL

49-31-00-710-001-A01

SYSTEMS

OPC

9

Perform a Check of the FADEC BITE display for fault messages

49-31-04-960-001-A00

SYSTEMS

DIS

9

Replace/Discard Inlet Fuel Filter.

49-31-04-960-001-A01

SYSTEMS

DIS

9

Replace/Discard APS 500R Inlet Fuel Filter

49-41-03-220-001-A00

SYSTEMS

DVI

6

Inspect (Detailed Inspection) Igniter Plug Ref a 49-44-03-200-801-A

P/N 816603-3 ONLY

PRE SB 145-36-0028 Applicable for APU MODEL T-62T-40C14 (APS500R). Discard Inlet Fuel Filter APU Model T-62T40C11 (APS 500)only Applicable for APU MODEL T-62T-40C14 (APS500R).

49-91-00-610-001-A00

SYSTEMS

SVC

6

49-91-00-680-001-A00

SYSTEMS

SVC

9

Drain and Replace Oil Supply Ref a 49-96-00-600-801-A

According to manufacturer's recommendation.

-

2000 AH

ALL

49-91-01-960-001-A00

SYSTEMS

DIS

9

Replace/Discard Oil Filter Element Ref a 49-96-01-960-801-A

According to manufacturer's recommendation.

-

2000 AH

ALL

71-20-00-220-001-A00

SYSTEMS

DVI

8

Inspect (Detailed Inspection) Engine Elastomeric Mounts

-

C

ALL

-

500 FH

ALL

-

10000 FH

ALL

-

10000 FH

ALL

72-00-00-200-801-001

ENGINE

GVI

Visually Inspect the air inlet section (fan assembly)

72-00-00-200-801-002

ENGINE

VCK

Visually inspect the accesory drives section.

72-00-00-200-801-003

ENGINE

VCK

Visually inspect bypass section.

Ref. Allison MM Section 5 Task 72-00-00-200801 Ref. Allison MM Section 5 Task 72-00-00-200801 Ref. Allison MM Section 5 Task 72-00-00-200801

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 13 -1- 4 .

SECCIÓN 13.TAREAS DE COMPONENTES REEMPLAZO MANTENIMIENTO LINEA "COMPONENT TASKS REPLACES BY LINE MAINTENANCE" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

72-00-00-200-801-004

ENGINE

VCK

Visually inspect fuel Cooled Oil Cooler

72-00-00-200-801-005

ENGINE

VCK

Visually inspect Fuel Sys Distribution

72-00-00-200-801-006

ENGINE

VCK

Visually inspect Oil Sys Distribution Ref. Allison MM Section 5

72-00-00-200-801-007

ENGINE

VCK

Visually inspect Power Control Ref. Allison MM Section 5

72-00-00-200-801-008

ENGINE

VCK

Visually inspect Turbine-inter stg (A) harness Ref. Allison MM Section 5

72-00-00-200-801-009

ENGINE

VCK

Visually inspect Turbine-Inter stg (B) harness Ref. Allison MM Section 5

72-21-01-220-001-A00

SYSTEMS

DVI

9

Inspect (Detailed Inspection) Fan Blades

72-21-20-220-001-A00

SYSTEMS

OPC

8

Inspect (detailed inspection) Fan Spinner Pre-Mod Rolls Royce SB 3007A-72-167 Only

Descripción / Description Ref. Allison MM Section 5 Task 72-00-00-200801 Ref. Allison MM Section 5 Task 72-00-00-200801 Ref. Allison MM Section 5 Task 72-00-00-200801 Ref. Allison MM Section 5 Task 72-00-00-200801 Ref. Allison MM Section 5 Task 72-00-00-200801 Ref. Allison MM Section 5 Task 72-00-00-200801 Ref. Allison MM Section 5 Task 72-21-15-200801

Ref. Allison MM Section 5 Task 72-63-10-700801 Applicable Post SB AE3007A-72-330 and Pre-Mod SB AE3007A-72-330 (All Aerolitoral ERJ-145 fleet) COMPLY AD 99-02-51 EXCEPT P/N: 23075904 and P/N: 23077006 ONLY RR Task 73-11-10-000-801 RR Task 7311-10-400-801 APPLICABLE TO P/N: 23075904 and P/N: 23077006 ONLY RR Task 73-11-10-000-801 RR Task 73-11-10-400-801 Ref. Allison MM Section 5 Task 74-21-10-200801 (All Aerolitoral ERJ-145 fleet) Applicable to aircraft WITH thrust reversers installed. And applicable only for P/N’s 83-990137, 83-990-152 and 83-990-166. COMPLY AD 2001-17-03 paragraph b)

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

10000 FH

ALL

-

10000 FH

ALL

-

10000 FH

ALL

-

10000 FH

ALL

-

10000 FH

ALL

-

10000 FH

ALL

-

4000 FH

ALL

-

A

ALL

-

800 FH

ALL

-

2000 FH

ALL

-

10000 FH

ALL

-

4000 FH

ALL

-

1200 FH

ALL

72-63-01-710-001-A00

SYSTEMS

OPC

AD

Operationally Check Starter Drain Adapter

73-11-10-130-001-A00

SYSTEMS

RST

6

Clean Fuel Nozzles

73-11-10-130-001-A01

SYSTEMS

RST

6

Clean Fuel Nozzles

74-21-01-220-001-A00

SYSTEMS

DVI

6

Inspect (Detailed Inspection) Ignitors

78-34-01-720-001-A00

SYSTEMS

FNC

AD

Functionally Check Stow/Transit Thrust Reverser Microswitches for insulation

79-25-02-211-001-A00

SYSTEMS

VCK

9

Visually Check Fuel Cooled Assembly (FCOC)

-

2C

ALL

79-27-00-211-001-A00

SYSTEMS

VCK

9

Visually Check Oil Plumbing

-

2C

ALL

A

ALL

-

2A

ALL

-

C

ALL

80-10-01-720-001-A00

SYSTEMS

FNC

6

Functionally check Air Turbine Starter including oil servicing

80-10-02-160-001-A00

SYSTEMS

SVC

6

Clean Start Control Valve Filter

To functionally check the air turbine Starter including oil servicing Applicable to Pre SB 145-80-0003 Only.

80-10-02-160-001-A01

SYSTEMS

SVC

6

Clean Start Control Valve Filter

Applicable to Post SB 145-80-0003 Only.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 14 -1-1 .

SECCIÓN 14.TAREAS DE COMPONENTES REEMPLAZO MANTENIMIENTO MAYOR "COMPONENT MAINTENANCE TASKS REPLEACES BY MAINTENENANCE MAYOR" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

32-10-01-900-001-A00

SYSTEMS

RST

8

20000 FC Or 144 MOS, whichever occurs first.

-

144 MOS

ALL

32-10-01-900-002-A00

SYSTEMS

RST

8

Or 20,000 FC, whichever occurs first.

-

144 MO

ALL

32-10-02-900-001-A00

SYSTEMS

RST

8

20000 FC Or 144 MOS, whichever occurs first.

-

144 MOS

ALL

32-10-03-900-001-A00

SYSTEMS

RST

8

32-10-03-900-002-A00

SYSTEMS

RST

8

20000 FC Or 144 MOS, whichever occurs first.

-

144 MOS

ALL

Or 20,000 FC, whichever occurs first.

-

144 MO

ALL

32-10-04-900-001-A00

SYSTEMS

RST

8

Restore MLG Secondary Side Strut, including spring cartridges (P/Ns 2309-2600-series)

20000 FC Or 144 MOS, whichever occurs first.

-

144 MOS

ALL

32-10-04-900-002-A00

SYSTEMS

RST

8

Restore MLG Lower Secondary Side Strut Assy

Or 20,000 FC, whichever occurs first.

-

144 MO

ALL

32-10-05-900-002-A00

SYSTEMS

RST

8

Or 20,000 FC, whichever occurs first.

-

144 MO

ALL

32-20-01-900-001-A00

SYSTEMS

RST

8

20000 FC Or 144 MOS, whichever occurs first.

-

144 MOS

ALL

32-20-01-900-002-A00

SYSTEMS

RST

8

Restore MLG Spring Cartridges Assy Restore Nose Landing Gear (NLG) Strut (P/N 1170b0000-series; 1170C0000-series; 2233A0000-series; and 2666A0000), including Torque Link, Steering cuff, sliding tube and web assy components; and their attaching parts Restore NLG Sliding Tube Assy

Or 20,000 FC, whichever occurs first.

-

144 MO

ALL

32-20-01-900-003-A00

SYSTEMS

RST

8

Restore NLG Steering Cuff Assy

Or 20,000 FC, whichever occurs first.

-

144 MO

ALL

32-20-01-900-004-A00

SYSTEMS

RST

8

-

ALL

32-20-02-900-001-A00

SYSTEMS

RST

8

32-20-02-900-002-A00

SYSTEMS

RST

8

32-20-03-900-001-A00

SYSTEMS

RST

8

Restore NLG Auxiliary Drag Strut Assy (P/Ns 1173b-series)

32-20-03-900-002-A00

SYSTEMS

RST

8

Restore NLG Lower Auxiliary Drag Strut Assy

Or 20,000 FC, whichever occurs first.

-

144 MO 20000 FC / 144 MOS 144 MO 20000 FC / 144 MOS 144 MO

ALL

32-20-04-900-002-A00

SYSTEMS

RST

8

Restore NLG Downlock Spring Assy

Or 20,000 FC, whichever occurs first.

-

144 MO

ALL

72-21-00-960-001-A00

SYSTEMS

DIS

6

Remove and Replace/Discard Fan Wheel and Fan Drive Shaft

(*) NOTE: • See Life-limit information Interval according to manufacturer's recommendation.

-

(*)

ALL

72-21-01-200-801

ENGINE

DVI

AD

Fan wheel Inspection

(*) NOTE: During each disassembly at engine shop Ref. Allison MM Section 5 COMPLY AD 2000-11-22

-

(*)

ALL

72-21-04-960-001-A00

SYSTEMS

DIS

6

Remove and Replace/Discard Fan Wheel Forward Retainer

(*) NOTE: • See Life-limit information. Interval according to manufacturer's recommendation.

-

(*)

ALL

Descripción / Description Restore Main Landing Gear (MLG) Leg Strut Assy (P/Ns 2309-2002series, 2309-3002-series, 2309-3100-series and-2309-4002-series) Restore MLG Trailing Arm Assy (P/Ns 2309-2037-series, 2309-3037series and 2309-4037-series), including wheel axle Restore MLG Shock Absorber Assy (P/Ns 2309-2005-series) Restore MLG Main Side Strut(P/Ns 2309-2500-series and 2309-3500series) Restore MLG Lower Main Side Strut Assy

Restore NLG Torque Link Assy Or 20,000 FC, whichever occurs first. Restore NLG Main Drag Strut (P/Ns 1172b0000-series and 1172C000020000 FC Or 144 MOS, whichever occurs first. series Restore NLG Main Drag Strut Bottom Stay Assy Or 20,000 FC, whichever occurs first. Or 20000 FC whichever occurs first.

-

ALL ALL ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 1 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

12-15-01-610-001-A00

SYSTEMS

SVC

REC

-

100 FH / 14 DY

ALL

20-00-00-212-011-A00

SYSTEMS

GVI

2C

EMB-145XR

20-00-00-220-005-A00

SYSTEMS

DET

2C

EMB-145XR

20-00-00-220-006-A00

SYSTEMS

DET

4C

EMB-145XR

21-26-08-960-001-A00

SYSTEMS

DIS

9

Discard Exhaust Hoses of the Electronic Bay Compartment.

Pre-Mod. SB 145-21-0013 (Not applicable Aerolitoral fleet)

-

5A

ALL

21-31-03-140-001-A01

SYSTEMS

RST

6

Clean Electropneumatic Outflow Valve

For smoking flights. (Not applicable Aerolitoral fleet)

-

2A

ALL

21-31-04-140-001-A01

SYSTEMS

RST

6

Clean Pneumatic Outflow Valve

For smoking flights. (Not applicable Aerolitoral fleet)

-

400 FH

ALL

21-31-08-960-001-A01

SYSTEMS

DIS

6

Replace Air Filter Element

-

1800 FH

ALL

22-11-00-720-003-A00

SYSTEMS

FNC

CAT II

Functionally Check Category II monitoring function

A8

800 FH

ALL

24-31-01-900-001-A00

SYSTEMS

RST

7

Restore Main Generator

-

3200 FH

ALL

24-34-01-900-001-A00

SYSTEMS

RST

7

Restore APU Starter/Generator

-

1200 AH

ALL

24-54-00-212-001-A00

SYSTEMS

GVI

7

Inspect (General Visual) PC Power Components

-

C

ALL

25-60-04-710-001-A00

SYSTEMS

OPC

8

Operationally Check Megaphone P/N ACR/EM-1A

25-60-04-960-001-A00

SYSTEMS

DIS

6

Discard of Megaphone Batteries P/N ACR/EM-1A

-

6 MO

ALL

-

12 MO

26-15-00-710-001-A00

ROUTINE

OPC

8

Operationally Check Baggage Smoke Detection System

ALL

-

100 FH / 14 DY

ALL

27-12-00-720-002-A00

SYSTEMS

FNC

8

27-12-00-720-003-A00

SYSTEMS

FNC

CMR

27-12-00-720-003-A01

SYSTEMS

FNC

CMR

Functionally Check Aileron Hydraulic Damping Functionally Check External Leakage of Aileron Hydraulic Actuator Functionally check external leakage of aileron hydraulic actuator

27-12-00-720-003-A05

SYSTEMS

FNC

8

27-12-01-212-002-A00

SYSTEMS

GVI

27-12-01-212-002-A01

SYSTEMS

GVI

27-12-01-212-002-A03

ROUTINE

GVI

27-12-01-212-002-A04

SYSTEMS

GVI

27-12-01-212-002-A07

SYSTEMS

GVI

27-12-01-720-001-A00

SYSTEMS

FNC

Descripción / Description Toilet Water Servicing Inspect (General Visual) Wing-to-fuselage attachment fairings XR model - EWIS Components of wiring bundles (Zones: 191, 193, 194, 195, 197, 198). NOTE: EWIS Inspect (Detailed Inspection) Ventral Fuel Tank - Electric Fuel Transfer Pump Connector (Zone: 196). NOTE: EWIS Inspect (Detailed Inspection) Ventral Fuel Tank - EWIS Components of Ventral Tank Unit Harness (Zone: 196). NOTE: EWIS

For smoking flights. (Not applicable All ERJ-145 Aerolitoral fleet) Maintenance Program Requirement for Cat. II Operation (Applicable until Aerolitoral Cat.II operation is certified) Applicable to P/N: 30086-010 ONLY Comply with task from SMRD 24-34-01-900-002A00 with int. 800 FH. The task from MRBR and SMRD are performed througt the same task from AMM 24-34-01-900-801-A. Applicable to aircraft equipped with PC Power System.

Applicable only for aircraft equipped with baggage compartment class "D" Pre S.B. 145-27-0062 Only

-

400 FH

EMB-145(ALL)

Pre-Mod SB 145-27-0063.

-

1500 FH

EMB-135 (ALL)

Post-Mod SB 145-27-0063

-

2500 FH

EMB-135 (ALL)

-

2A

EMB-145(ALL)

-

500 FH

EMB-135 (ALL)

-

1000 FH

EMB-135 (ALL)

-

100 FH / 14 DY

EMB-145 (ALL)

-

25 FH / 3 DY

EMB-145(ALL)

-

2A

EMB-145(ALL)

-

500 FH

EMB-135 (ALL)

Functionally check External Leakage of Aileron Hydraulic Actuator for aircraft Certificated Under EASA Regulations

Inspect (Visual Inspection) Aileron PCA Rod Ends/Fitting Lugs Pre-Mod SB 145-27-0063 (Not applicable Aerolitoral fleet) for Integrity and General Condition. Post-Mod SB 145-27-0063 (Not applicable Inspect (Visual Inspection) Aileron PCA Rod Ends/Fitting Lugs CMR Aerolitoral fleet) for Integrity and General Condition. Inspect (Visual Inspection) Aileron PCA Rod Ends/Fitting 8 Applicable for P/N: 394900-1007 ONLY Lugs for Integrity and General Condition 25 FH / 3 Days for a/c equipped with PCA PN Inspect (Visual Inspection) Aileron PCA Rod Ends/Fitting Lugs 8 394900-1003 or PN 394900-1005 ONLY (Not for Integrity and General Condition. applicable Aerolitoral ERJ145 fleet) (*) NOTE: "2A" - Post-Mod SB145-27-0061/-62 & Inspect (Visual Inspection) Aileron PCA Rod Ends/Fitting Lugs SB145-57-0019 (Applicable to aircraft under EASA 8 for Integrity and General Condition. Regulations) (Not applicable All Aerolitoral ERJ145 fleet) Functionally Check Aileron Actuator Damping Components Applicable to aircraft Post-Mod SB 145-27-0062 and CMR Pre-Mod SB 145-27-0063 and Monitoring Devices CMR

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 2 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

27-12-01-720-001-A01

SYSTEMS

FNC

CMR

Functionally Check Aileron Actuator Damping Components and Monitoring Devices

27-12-01-720-001-A05

SYSTEMS

FNC

8

Functionally Check Aileron Actuator Damping Components and Monitoring Devices

27-12-01-720-002-A02

SYSTEMS

FNC

9

Functionally Check Aileron Actuator Force Fight.

27-12-03-212-001-A00

SYSTEMS

VCK

CMR

Inspect (Visual Inspection) Aileron Damper Rod Ends/Fitting Lugs for Integrity and General Condition.

27-12-03-720-001-A00

SYSTEMS

FNC

CMR

Functionally Check Aileron Damper Damping Force

27-12-03-720-002-A00

SYSTEMS

FNC

CMR

Functionally Check External Leakage of aileron damper

27-40-00-720-003-A00

SYSTEMS

FNC

9

27-51-00-610-001-A01

SYSTEMS

SVC

6

27-70-00-710-001-A00

SYSTEMS

OPC

7

Functional Check Mach Trim Function Service Flap Screw-jack Actuators Gearbox POST-MOD SB 145-27-0118 Operationally Check Mechanical Gust Lock Mechanism

27-70-00-720-001-A00

SYSTEMS

FNC

9

Functionally check the Gap of Elevator Secondary Stop.

28-17-01-720-001-A00

SYSTEMS

FNC

28-17-03-710-001-A00

SYSTEMS

OPC

9

Functionally Check critical bonding integrity of Fuel pump, VFQIS and Low Level SW connectors at tank wall by conductivity measurements. Operationally Check Ventral Fuel Tank Flap Valves

28-17-04-710-001-A00

SYSTEMS

OPC

9

Operationally Check Ventral Fuel Tank Baffle Valves

28-18-01-710-001-A00

SYSTEMS

OPC

9

28-18-03-710-001-A00

SYSTEMS

OPC

9

28-18-05-211-001-A00

SYSTEMS

VCK

9

Operationally Check Ventral Fuel Tank Float Vent Valves Operationally Check Ventral Fuel Tank Float Actuated Drain Valve Visually Check Ventral Fuel Tank Flame Arrestor

28-27-00-710-001-A00

SYSTEMS

OPC

9

Operationally Check Ventral Fuel Tank Transfer System

Descripción / Description

Inspect Electric Fuel Transfer Pump Connector

Applicable to aircraft Post-Mod SB 145-27-0062 and Post-Mod SB 145-27-0063 Applicable to aircraft Post-Mod SB 145-27-0062 for aircraft under EASA Regulations (Not applicable All Aerolitoral ERJ-145 fleet) Applicable to aircraft Post-Mod SB 145-27-0062 under EASA Regulations. (Not applicable All Aerolitoral ERJ145 fleet) Applicable to aircraft Post-Mod SB 145-27-0063 under CTA/FAA certifications. Applicable to aircraft Post-Mod SB 145-27-0063, under CTA/FAA certifications. Post-Mod SB 145-27-0063

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

2500 FH

EMB-135 (ALL)

-

2A

EMB-145(ALL)

-

2A

EMB-145(ALL)

-

1000 FH

EMB-135 (ALL)

-

2500 FH

EMB-135 (ALL)

-

2500 FH

EMB-135 (ALL)

-

C

EMB-145XR

-

2C

ALL

Mechanical Gust Lock System ONLY Mechanical Gust Lock System ONLY Pre-Mod. S.B. 145-27-0079

-

C

ALL

-

4000 FH

ALL

Comply BAD 2007-08-02 AND AD 2008-13-14

-

30000 FH

EMB-145XR

-

2C

EMB-145XR

-

2C

EMB-145XR

-

2C

EMB-145XR

Applicable to all Aerolitoral ERJ145 fleet Comply BAD 2000-08-01R3 Comply BAD 2007-08-02 AND AD 2008-13-14

-

2C

EMB-145XR

-

C

EMB-145XR

-

2A

EMB-145XR

-

10000 FH

EMB-145XR

28-27-01-220-001-A00

SYSTEMS

DET

28-27-06-710-001-A00

SYSTEMS

OPC

9

Operationally Check Transfer Float Shutoff Valve

-

2C

EMB-145XR

28-27-10-710-001-A00

SYSTEMS

OPC

8

Operationally Check Fuel Transfer Line Shroud

-

2C

EMB-145XR

28-41-00-710-002-A00

SYSTEMS

OPC

9

Operationally Check Electrical Fuel Quantity Indicating System

-

C

EMB-145XR

28-41-00-720-001-A00

SYSTEMS

FNC

9

Functionally Check Electrical Fuel Quantity Indicating System

28-41-04-720-001-A00

SYSTEMS

FNC

28-41-07-220-001-A00

SYSTEMS

DET

Functionally Check Ventral Fuel conditioning Unit (FCU) Inspect VFQIS and Low Level SW Harness for clamp and wire jacket integrity

28-50-03-220-001-A00

SYSTEMS

DET

8

Inspect (Detailed Inspection) Ventral Tank Unit

30-41-00-710-001-A00

SYSTEMS

OPC

CAT II

Operationally Check Windshield Wiper

30-44-04-720-001-A00

SYSTEMS

FNC

REC

Functionally Check Rain Repellent Coating (RRC)

32-34-00-720-001-A00

SYSTEMS

FNC

8

Functionally Check Landing Gear Emergency Extension

33-11-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Cockpit Lights

C

EMB-145XR

Comply BAD 2007-08-02 AND AD 2008-13-14

-

10000 FH

EMB-145XR

Comply BAD 2007-08-02 AND AD 2008-13-14

20000 FH

EMB-145XR

2C

EMB-145XR

NOTE: This task complies with Fuel Tank Ignition Source Prevention (SFAR 88). Maintenance Program Requirement for Cat. II Operation (Applicable until Aerolitoral Cat.II operation is certified) If installed

A8

C

ALL

-

A

ALL

"A" to aircraft Pre-Mod. SB 145-32-0036 and 145-320037. (Not applicable All Aerolitoral ERJ145 fleet)

-

A

ALL

-

C

ALL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 3 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

33-12-00-710-001-A00

SYSTEMS

OPC

REC

33-15-00-710-001-A00

SYSTEMS

OPC

REC

33-21-00-710-001-A00

SYSTEMS

OPC

REC

33-23-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Passenger Warning Signs

-

C

ALL

33-25-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Reading and Attendant Call Lights

-

C

ALL

33-26-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Courtesy/Stair Lights

-

C

ALL

33-28-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Lavatory Lights

-

C

ALL

33-29-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Galley Lights

-

C

ALL

33-30-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Baggage and Service Compartments

-

C

ALL

33-41-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Landing Lights

-

C

ALL

33-42-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Taxi Lights

-

C

ALL

33-43-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Navigation Lights

-

C

ALL

33-44-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Inspection Lights

-

C

ALL

33-46-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Logotype Lights

-

C

ALL

33-47-00-710-001-A00

SYSTEMS

OPC

REC

Operationally Test Anti-collision Lights

-

C

ALL

-

C

ALL

-

C

ALL

-

C

ALL

-

C

ALL

34-13-00-680-001-A00

SYSTEMS

SVC

6

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

Operationally Test Instrument and Control Panel Lighting

-

C

ALL

Operationally Test Flood/Storm Lights

-

C

ALL

Operationally Test Passenger Cabin Lights

-

C

ALL

Descripción / Description

Drain Pitot Lines

Pre-Mod SB 145-34-0021 Only (Not Applicable All Aerolitoral ERJ145 fleet)

Inspect (Special Inspection) RVSM Critical Region (Skin) for Waviness (including aircraft identified in and are Post-Mod SB 145-34-0110). Inspect (Special Inspection) Static Port Surrounding Plate for Flushness and Integrity (including aircraft identified in and are Post-Mod SB 145-34-0110). Inspect (Special Inspection) Passenger Gaseous Oxygen Service Panel (panel P/N 145-51705-001, attached by livelock stud xnut) installed in RVSM critical region for Flushness and Integrity (including aircraft identified in and are Post-Mod SB 145-34-0110).

34-13-04-280-001-A01

SYSTEMS

SDI

6

34-13-04-280-002-A01

SYSTEMS

SDI

6

34-13-04-280-003-A01

SYSTEMS

SDI

6

34-41-00-710-001-A00

SYSTEMS

OPC

CAT II

Operationally Check GPWS/Windshear

Maintenance Program Requirement for Cat. II Operation

-

C

ALL

35-21-00-211-001-A00

SYSTEMS

VCK

8

Visually Check Pressure Indication Between MFD Versus Cylinder Gauge and Charging Gauge Versus Cylinder Gauge

NOTE: Aircraft Equipped with Gaseous Oxygen System (Shuttle Configuration Only).

-

4A

EMB-135LR

35-21-00-710-001-A00

SYSTEMS

OPC

8

Operationally Check Passenger Oxygen System in MANUAL Mode

-

4A

EMB-135LR

35-21-00-710-002-A00

SYSTEMS

OPC

8

Operationally Check "VLV CLOSED" Indication Circuit

NOTE: Aircraft Equipped with Gaseous Oxygen System (Shuttle Configuration Only). NOTE: Aircraft Equipped with Gaseous Oxygen System (Shuttle Configuration Only). NOTE: Aircraft Equipped with Gaseous Oxygen System (Shuttle Configuration Only). NOTE: Aircraft Equipped with Gaseous Oxygen System (Shuttle Configuration Only). NOTE: Aircraft Equipped with Gaseous Oxygen System (Shuttle Configuration Only). NOTE: Aircraft Equipped with Gaseous Oxygen System (Shuttle Configuration Only). NOTE: Aircraft Equipped with Gaseous Oxygen System (Shuttle Configuration Only). NOTE: Aircraft Equipped with Gaseous Oxygen System (Shuttle Configuration Only).

-

4A

EMB-135LR

-

C

EMB-135LR

-

C

EMB-135LR

-

4A

EMB-135LR

-

36 MOS

EMB-135LR

-

180 MOS

EMB-135LR

-

4A

EMB-135LR

35-21-00-710-003-A00

SYSTEMS

OPC

8

Operationally Check "PAX OXY LOW PRESS" Caution Message

35-21-00-720-001-A00

SYSTEMS

FNC

8

Functionally Check Passenger Oxygen System in AUTO Mode

35-21-02-211-001-A00

SYSTEMS

VCK

8

Visually Check Passenger Oxygen Mask Assy

35-21-04-720-001-A00

SYSTEMS

FNC

8

Functionally Check (Hydrostatic Test) Passenger Oxygen Cylinder

35-21-04-960-001-A00

SYSTEMS

DIS

8

Replace/Discard Passenger Oxygen Cylinder

35-21-06-710-001-A00

SYSTEMS

OPC

8

Operationally Check Electric Pulse/Latching On-Off Valve

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 4 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

35-21-07-720-001-A00

SYSTEMS

FNC

8

Functionally Check of Oxygen Sequence Regulator

35-21-15-710-001-A00

SYSTEMS

OPC

8

Check (Leak) Passenger Oxygen Distribution (HP) Lines

35-21-16-710-001-A00

SYSTEMS

OPC

8

Check (Leak) Passenger Oxygen Distribution (LP) Lines

-

C

EMB-135LR

36-11-11-710-001-A00

SYSTEMS

OPC

9

Operationally Check Thermostat Shutoff Valve

-

C

EMB-145XR

38-30-00-610-001-A00

SYSTEMS

SVC

REC

Toilet Waste Bowl Servicing

-

100 FH / 14 DY

ALL

45-45-00-970-001-A00

SYSTEMS

DRC

REC

-

100 FH / 14 DY

52-10-00-220-802-A00

STRUCTURAL

DET

-

Only aircraft equipped with STANDARD MAIN DOOR model.

20000 FC

10000 FC

52-10-00-220-803-A00

STRUCTURAL

DET

-

CMC DATA - MFD Downloading Internally inspect the MAIN DOOR (STANDARD MODEL) components: • Attachment fittings-to-fuselage & interface parts (SSI 52-10-05) Externally inspect the MAIN DOOR (STANDARD MODEL) components: • Attachment fittings-to-fuselage & interface parts (SSI 52-10-05)

Only aircraft equipped with STANDARD MAIN DOOR model.

20000 FC

5000 FC

52-10-00-220-803-A01

STRUCTURAL

DET

-

Externally inspect the MAIN DOOR (SIDE-HINGED MODEL) components: • Stop & backup structures (SSI 52-10-03)

Only aircraft equipped with SIDE HINGED MAIN DOR model.

20000 FC

2502 FC

52-10-00-220-804-A00

STRUCTURAL

DET

-

Externally inspect the MAIN DOOR (STANDARD MODEL) components: • Stop & backup structures (SSI 52-10-03)

Only aircraft equipped with STANDARD MAIN DOOR model.

20000 FC

2502 FC

52-10-00-220-804-A01

STRUCTURAL

DET

-

Internally inspect the MAIN DOOR (SIDE-HINGED MODEL) components: • Stop & backup structures (SSI 52-10-03)

Only aircraft equipped with SIDE HINGED MAIN DOR model.

20000 FC

4447 FC

52-10-00-220-805-A00

STRUCTURAL

DET

-

Internally inspect the MAIN DOOR (STANDARD MODEL) components: • Stop & backup structures (SSI 52-10-03)

Only aircraft equipped with STANDARD MAIN DOOR model.

20000 FC

5000 FC

52-21-00-220-801-A00

STRUCTURAL

DET

-

Externally inspect the PASSENGER CABIN ESCAPE HATCH components: • Escape hatch structure (SSI 52-21-06)

19000 FC

5000 FC

52-21-00-220-802-A00

STRUCTURAL

DET

-

Internally inspect the PASSENGER CABIN ESCAPE HATCH components: • Escape hatch structure (SSI 52-21-06)

19000 FC

5060 FC

52-21-00-220-803-A00

STRUCTURAL

DET

-

Internally inspect the PASSENGER CABIN ESCAPE HATCH components: • Escape hatch window frame (SSI 52-21-07)

20000 FC

6060 FC

52-30-00-220-801-A00

STRUCTURAL

DET

-

Internally inspect the BAGGAGE DOOR components: • Baggage door stops and fittings (SSI 52-30-09)

20000 FC

4318 FC

52-43-00-220-802-A00

STRUCTURAL

DET

-

Externally inspect the SERVICE DOOR components: • Service door folding flap stops (SSI 52-43-14)

20000 FC

4975 FC

52-43-00-220-804-A00

STRUCTURAL

DET

-

Externally inspect the SERVICE DOOR components: • Service door stops & backup structure (SSI 52-43-13)

20000 FC

2465 FC

52-43-00-220-805-A00

STRUCTURAL

DET

-

Internally inspect the SERVICE DOOR components: • Service NOTE: During this inspection, the CPCP basic task door stops & backup structure (SSI 52-43-13) shall also be performed for this SSI.

20000 FC

4640 FC

52-43-00-220-806-A00

STRUCTURAL

DET

-

Internally inspect the SERVICE DOOR components: • Service NOTE: During this inspection, the CPCP basic task door folding flap stops (SSI 52-43-14) shall also be performed for this SSI.

20000 FC

5000 FC

53-11-00-220-801-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE component: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-1007)

20000 FC

10000 FC

ALL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

Descripción / Description NOTE: Aircraft Equipped with Gaseous Oxygen System (Shuttle Configuration Only). NOTE: Aircraft Equipped with Gaseous Oxygen System (Shuttle Configuration Only). NOTE: Aircraft Equipped with Gaseous Oxygen System (Shuttle Configuration Only).

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

4A

EMB-135LR

-

C

EMB-135LR

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 5 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

53-11-00-220-802-A00

STRUCTURAL

DET

-

53-11-00-220-806-A00

STRUCTURAL

DET

-

53-11-00-220-C06-A00

CORROSION PROGRAM

DET

CPCP

Descripción / Description Internally Inspect the FUSELAGE components • Forward bulkhead (SSI 53-10-26) Internally inspect the FUSELAGE components: • Longerons (SSI 53-10-46) Internally inspect the FUSELAGE components: • Longerons (SSI 53-10-46)

53-12-00-220-805-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Windshield lateral post and its attachment (SSI 53-10-20)

53-12-00-220-808-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Windshield center post, including its attachments and lower fitting (SSI 5310-19)

53-12-00-220-808-A01

STRUCTURAL

DET

-

53-12-00-220-812-A00

STRUCTURAL

DET

-

53-12-00-220-813-A00

STRUCTURAL

DET

-

53-12-00-220-814-A00

STRUCTURAL

DET

-

53-21-00-210-801-A00

STRUCTURAL

GVI

-

53-21-00-220-802-A00

STRUCTURAL

DET

-

53-21-00-220-803-A00

STRUCTURAL

DET

-

53-21-00-220-814-A00

STRUCTURAL

DET

-

53-21-00-220-816-A00

STRUCTURAL

DET

53-21-00-220-817-A00

STRUCTURAL

53-21-00-220-818-A00

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

18000 FC

10000 FC

EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

19737 FC

EMB-145XR

-

96 MOS

EMB-145XR EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

6666 FC

12000 FC

4000 FC

20000 FC

10000 FC

12000 FC

12000 FC

EMB-145XR

12000 FC

12000 FC

EMB-145XR

-

12929 FC

EMB-145XR

10000 FC

5000 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

3735 FC

20000 FC

5000 FC

Externally inspect the FUSELAGE components: • Passenger cabin window frame (SSI 53-20-06)

20000 FC

2500 FC

-

Externally inspect the FUSELAGE components: • Frame 15 & 18 LHS splices at stringers 3L & 16L (SSI 53-20-12)

20000 FC

2764 FC

DET

-

Externally inspect the FUSELAGE components: • Stringer 6 & 16 splices at frames 20 & 22 (SSI 53-20-13)

20000 FC

2764 FC

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Passenger cabin window frame (SSI 53-20-06)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

20000 FC

5000 FC

53-21-00-220-821-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage NOTE: During this inspection, the CPCP basic task skin longitudinal splices along main door cutout (SSI 53-20-41) shall also be performed for this SSI.

20000 FC

4932 FC

53-21-00-220-822-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage NOTE: During this inspection, the CPCP basic task skin longitudinal splices along service door cutout (SSI 53-20shall also be performed for this SSI. 42)

20000 FC

5000 FC

53-21-00-220-828-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: Frame 15 & 18 NOTE: During this inspection, the CPCP basic task LHS splices at stringers 3L& 16L (SSI 53-20-12) shall also be performed for this SSI.

20000 FC

2979 FC

53-21-00-220-829-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: Stringer 6 & 16 NOTE: During this inspection, the CPCP basic task splices at frames 20 & 22 (SSI 53-20-13) shall also be performed for this SSI.

20000 FC

2979 FC

NOTE: Applicable to aircraft Pre-Mod. SB 145-530007.

Internally inspect the FUSELAGE components: • Windshield NOTE: Applicable to aircraft Post -Mod. SB 145-53center post, including its attachments and lower fitting (SSI 530007. 10-19) Internally inspect the FUSELAGE components: • Windshield cutout structure (SSI 53-10-17) Internally inspect the FUSELAGE components: • Windshield cutout structure (SSI 53-10-17) Internally inspect the FUSELAGE components: • Windshield center Post, including its attachment and lower fitting (SSI 5310-19) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5320-07). Externally inspect the FUSELAGE components: • Stops and backup structures for main door (SSI 53-20-01) Internally inspect the FUSELAGE components: • Stops and NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. backup structure for main door (SSI 53-20-01)

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; F-GAC-01 EMB-135KL SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 6 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

53-21-00-220-830-A00

STRUCTURAL

DET

-

53-21-00-220-831-A00

STRUCTURAL

DET

-

53-21-00-220-832-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: Passenger door cutout reinforcing structures (SSI 53-20-09)

53-21-00-220-833-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: Passenger door cutout reinforcing structures (SSI 53-20-09)

53-21-00-220-834-A00

STRUCTURAL

DET

-

53-21-00-220-835-A00

STRUCTURAL

DET

-

53-21-00-220-836-A00

STRUCTURAL

DET

-

53-21-00-220-837-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Fuselage skin longitudinal splices allow main door cutout (SSI 53-20-41)

53-21-00-220-838-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage NOTE: During this inspection, the CPCP basic task skin longitudinal splices allow main door cutout (SSI 53-20-41) should also be performed for this SSI

53-21-00-220-840-A00

STRUCTURAL

DET

-

53-21-00-220-841-A00

STRUCTURAL

DET

-

53-21-00-220-843-A00

STRUCTURAL

DET

-

53-21-00-220-844-A00

STRUCTURAL

DET

-

53-21-00-220-845-A00

STRUCTURAL

DET

-

53-22-00-210-801-A00

STRUCTURAL

GVI

-

53-22-00-210-803-A00

STRUCTURAL

GVI

-

53-22-00-210-804-A00

STRUCTURAL

GVI

-

53-22-00-220-801-A00

STRUCTURAL

DET

-

53-22-00-220-805-A00

STRUCTURAL

DET

-

53-23-00-210-803-A00

STRUCTURAL

GVI

-

53-23-00-210-804-A00

STRUCTURAL

GVI

-

Descripción / Description Internally inspect the FUSELAGE components: Fuselage panels at Stringers, frames / Bulkheads, and splices (SSI 5320-07). Internally inspect the FUSELAGE components: Fuselage skin panels at Stringers, frames / Bulkheads, and splices (SSI 5320-07).

Internally inspect the FUSELAGE components: Service door cutout reinforcing structures (SSI 53-20-10) Externally inspect the FUSELAGE components: Service door cutout reinforcing structures (SSI 53-20-10) Internally inspect the FUSELAGE components: Frames (SSI 53-20-43)

NOTE: During this inspection, the CPCP basic task should also be performed for this SSI.1

NOTE: Remove the bumper plate if installed

Internally inspect the FUSELAGE components: • Stops and NOTE: During this inspection, the CPCP basic task should also be performed for this SSI backup structure for main door (SSI 53-20-01) Externally inspect the FUSELAGE components: • Stops and backup structure for main door (SSI 53-20-01) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5320-07) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5320-07) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5320-07) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5320-07) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringer, frames/bulkheads, and splices (SSI 5320-07) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringer, frames/bulkheads, and splices (SSI 5320-07) Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5320-07) Internally Inspect the FUSELAGE components: • Fuselage skin circumferential splice (SSI 53-20-14) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5320-07) Externally inspect the FUSELAGE components: • Passenger cabin window frame (SSI 53-20-06)

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

-

10000 FC

EMB-145XR

-

10000 FC

EMB-145XR

19000 FC

5000 FC

EMB-145XR

19000 FC

5000 FC

EMB-145XR

20000 FC

5000 FC

EMB-145XR

20000 FC

5000 FC

EMB-145XR

-

10000 FC

EMB-145XR

-

5000 FC

EMB-145XR

20000 FC

4965 FC

EMB-145XR

20000 FC

5000 FC

EMB-145XR

20000 FC

4180 FC

EMB-145XR

20000 FC

5000 FC

EMB-145XR

18000 FC

5000 FC

EMB-145XR

7000 FC

5000 FC

EMB-145XR

20000 FC

2500 FC

EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

2500 FC

EMB-145XR

20000

3831 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

10000 FC

EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

8102 FC

EMB-145XR

20000 FC

3388 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

4125 FC

EMB-145XR F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 7 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

53-23-00-220-801-A00

STRUCTURAL

DET

-

53-23-00-220-802-A00

STRUCTURAL

DET

-

53-23-00-220-803-A00

STRUCTURAL

DET

-

53-23-00-220-806-A00

STRUCTURAL

DET

-

53-23-00-220-810-A00

STRUCTURAL

DET

-

53-23-00-220-811-A00

STRUCTURAL

DET

-

53-23-00-220-812-A00

STRUCTURAL

DET

-

53-23-00-220-813-A00

STRUCTURAL

DET

-

53-23-00-220-814-A00

STRUCTURAL

DET

-

53-23-00-220-815-A00

STRUCTURAL

DET

-

53-23-00-220-816-A00

STRUCTURAL

DET

53-23-00-220-817-A00

STRUCTURAL

DET

53-24-00-210-803-A00

STRUCTURAL

GVI

53-24-00-210-806-A00

STRUCTURAL

GVI

53-24-00-210-807-A00

STRUCTURAL

GVI

53-24-00-210-808-A00

STRUCTURAL

GVI

53-24-00-210-810-A00

STRUCTURAL

GVI

53-24-00-210-C07-A00

CORROSION PROGRAM

GVI

53-24-00-210-C09-A00

CORROSION PROGRAM

GVI

CPCP

53-24-00-210-C09-A01

CORROSION PROGRAM

GVI

CPCP

Descripción / Description NOTE: During this inspection, the CPCP basic task Internally inspect the FUSELAGE components: • Fuselage shall also be performed for this SSI. machined bulkhead (SSI 53-20-30) Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5320-07) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5320-07) Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5320-07) Internally inspect the FUSELAGE components: • Machined frame at ventral fuel tank attachment points (SSI 53-20-84) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5320-07) Internally inspect the FUSELAGE components: • Fuselage machined bulkhead (SSI 53-20-30) NOTE: During this inspection, the CPCP basic task Internally inspect the FUSELAGE components: • Fuselage shall also be performed for this SSI. machined bulkhead (SSI 53-20-30) Internally inspect the FUSELAGE components: • Fuselage machined bulkhead (SSI 53-20-30)

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

20000 FC

10000 FC

EMB-145XR

20000 FC

10000 FC

EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

6140 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

20000 FC

EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

10000 FC

EMB-145XR

20000 FC

5000 FC

EMB-145XR

-

10000 FC

EMB-145XR EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

9167 FC

20000 FC

9443 FC

-

4725 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

10000 FC

EMB-145XR

20000 FC

6428 FC

EMB-145XR

20000 FC

5000 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

12000 FC

4750 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

19000 FC

3077 FC

EMB-145XR

-

10000 FC

EMB-145XR

-

5543 FC

EMB-145XR

-

60 MOS

EMB-145XR

Externally inspect the VENTRAL FUEL TANK component: • Frontal Side of Ventral Fuel tank structure (SSI 53-20-87) NOTE: Applicable to aircraft Pre-Mod. SB 145-53-0074.

30 MOS

EMB-145XR

Externally inspect the VENTRAL FUEL TANK component: • Frontal Side of Ventral Fuel tank structure (SSI 53-20-87) NOTE: Applicable to aircraft Post-Mod. SB 145-53-0074.

30 MOS

EMB-145XR

Externally inspect the FUSELAGE components: • Skin and reinforcement around escape hatch cutout (SSI 53-20-51)

Externally inspect the FUSELAGE components: • Overwing fuselage skin panel (SSI 53-20-16) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5320-07) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices.(SSI 5320-07) Externally inspect the FUSELAGE components: fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-2007) Externally inspect the FUSELAGE components: fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-2007) Externally inspect the FUSELAGE components: fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-2007) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5320-07) Externally inspect the VENTRAL FUEL TANK components: • CPCP Ventral fuel tank structure (SSI 53-20-85) -

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 8 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

53-24-00-220-801-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5320-07)

53-24-00-220-803-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: Machined frame at ventral fuel tank attachment points (SSI 53-20-84)

53-24-00-220-805-A00

STRUCTURAL

DET

53-24-00-220-809-A00

STRUCTURAL

DET

53-24-00-220-C05-A00 53-24-00-220-C08-A00

CORROSION PROGRAM CORROSION PROGRAM

DET DET

Descripción / Description Not applicable to aircrafts model MP

Externally inspect the VENTRAL FUEL TANK components: • Ventral fuel tank attachment points, including main bolts (SSI 53-20-86) Internally inspect the FUSELAGE components: • Fuselage skin circumferential splice (SSI 53-20-14) Internally inspect the VENTRAL FUEL TANK components: • CPCP Ventral fuel tank structure (SSI 53-20-85) Internally inspect the FUSELAGE components: • fuselage skin CPCP circumferential splice (SSI 53-20-14) -

53-24-00-220-c09-a00

CORROSION PROGRAM

DET

CPCP

53-31-00-210-802-A00

STRUCTURAL

GVI

-

53-31-00-210-804-A00

STRUCTURAL

GVI

-

53-31-00-210-805-A00

STRUCTURAL

GVI

-

53-31-00-210-806-A00

STRUCTURAL

GVI

-

53-31-00-210-812-A00

STRUCTURAL

GVI

-

53-31-00-210-813-A00

STRUCTURAL

GVI

-

53-31-00-210-814-A00

STRUCTURAL

GVI

-

53-31-00-210-815-A00

STRUCTURAL

GVI

-

53-31-00-210-816-A00

STRUCTURAL

GVI

-

53-31-00-210-817-A00

STRUCTURAL

GVI

-

53-31-00-210-818-A00

STRUCTURAL

GVI

-

53-31-00-210-819-A00

STRUCTURAL

GVI

-

53-31-00-210-820-A00

STRUCTURAL

GVI

-

53-31-00-210-C02-A00

CORROSION PROGRAM

GVI

CPCP

53-31-00-220-802-A00

STRUCTURAL

DET

-

53-31-00-220-804-A00

STRUCTURAL

DET

-

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

20000 FC

10000 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL; EMB-145XR

-

10000 FC

EMB-145XR

-

9958 FC

EMB-145XR

-

10000 FC

EMB-145XR

-

60 MOS

EMB-145XR

-

60 MOS

EMB-145XR

30 MOS

EMB-145XR

20000 FC

5000 FC

EMB-135ER; EMB-135LR EMB-135KE; EMB-135KL

20000 FC

10000 FC

20000

10000

20000 FC

10000 FC

20000 FC

5000 FC

-

5000 FC

EMB-145XR

-

10000 FC

EMB-145XR

-

10000 FC

EMB-145XR

-

5000 FC

EMB-145XR

-

10000 FC

EMB-145XR

-

10000 FC

EMB-145XR

-

5000 FC

EMB-145XR

-

10000 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

30 MOS

EMB-135ER EMB-135LR

20000 FC

10000 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

10000 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

Internally inspect the VENTRAL FUEL TANK components: • Frontal Side of Ventral Fuel tank structure (SSI 53-20-87) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5330-07) Externally inspect the FUSELAGE components: • Fuselage skin panel at pressure bulkhead (SSI 53-30-15) Externally inspect the FUSELAGE components: • Fuselage skin panel at pressure bulkhead (SSI 53-30-15) Externally inspect the FUSELAGE components: • Fuselage machined bulkhead (SSI 53-30-30) Externally inspect the FUSELAGE components: • Fuselage skin panel at pressure bulkhead (SSI 53-30-15) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5330-07) Externally inspect the FUSELAGE components: • Fuselage skin panel at pressure bulkhead (SSI 53-30-15) Externally inspect the FUSELAGE components: • Fuselage skin panel at pressure bulkhead (SSI 53-30-15) Externally inspect the FUSELAGE components: • Fuselage skin panel at pressure bulkhead (SSI 53-30-15) Internally inspect the FUSELAGE components: • Baggage compartment floor beams and columns (SSI 53-30-28) Externally inspect the FUSELAGE components: • Fuselage machined bulkhead (SSI 53-30-30) Externally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5330-07) Externally inspect the FUSELAGE components: • Baggage Compartment floor beams and columns (SSI 53-30-15) Externally inspect the FUSELAGE components: • Toilet waste drain valve support (SSI 53-30-29) Internally inspect the FUSELAGE components: • Fuselage skin panel at pressure bulkhead (SSI 53-30-15) Internally inspect the FUSELAGE components: • Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 5330-07)

Remove the bumper plate, if is installed

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 9 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

53-31-00-220-806-A00

STRUCTURAL

DET

-

14000 FC

10000 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

53-31-00-220-811-A00

STRUCTURAL

DET

-

20000 FC

5000 FC

53-31-00-220-812-A00

STRUCTURAL

DET

-

20000 FC

8778 FC

53-31-00-220-813-A00

STRUCTURAL

DET

-

20000 FC

10000 FC

53-31-00-220-814-A00

STRUCTURAL

DET

-

20000 FC

10000 FC

53-31-00-220-815-A00

STRUCTURAL

DET

-

20000 FC

6256 FC

53-31-00-220-820-A00

STRUCTURAL

DET

-

14000 FC

10000 FC

53-31-00-220-823-A00

STRUCTURAL

DET

-

-

2228 FC

53-31-00-220-824-A00

STRUCTURAL

DET

-

-

4038 FC

EMB-145XR

53-31-00-220-825-A00

STRUCTURAL

DET

-

-

8778 FC

EMB-145XR

53-31-00-220-826-A00

STRUCTURAL

DET

-

-

5468 FC

EMB-145XR

53-31-00-220-827-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Rear electronic compartment door cutout structure (SSI 53-30-49)

-

5735 FC

EMB-145XR

53-31-00-220-828-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: Rear electronic compartment door cutout structure (SSI 53-30-49)

-

6340 FC

EMB-145XR

53-31-00-220-829-A00

STRUCTURAL

DET

-

-

10000 FC

EMB-145XR

53-31-00-220-830-A00

STRUCTURAL

DET

-

-

10000 FC

EMB-145XR

53-31-00-220-831-A00

STRUCTURAL

DET

-

-

5000 FC

EMB-145XR

53-31-00-220-832-A00

STRUCTURAL

DET

-

-

10000 FC

EMB-145XR

53-31-00-220-833-A00

STRUCTURAL

DET

-

-

10000 FC

EMB-145XR

53-31-00-220-834-A00

STRUCTURAL

DET

-

-

8003 FC

EMB-145XR

53-31-00-220-835-A00

STRUCTURAL

DET

-

-

4115 FC

EMB-145XR

53-31-00-220-836-A00

STRUCTURAL

DET

-

-

10000 FC

EMB-145XR

53-31-00-220-838-A00

STRUCTURAL

DET

-

Externally inspect the FUSELAGE components: • Rear electronic compartment door cutout structure (SSI 53-30-49)

12000 FC

4520 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

53-31-00-220-841-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Baggage door lateral L-shape (SSI 53-30-03)

-

5468 FC

EMB-145XR

53-31-00-220-842-A00

STRUCTURAL

DET

-

Internally inspect the FUSELAGE components: • Rear electronic compartment door cutout structure (SSI 53-30-49)

12000 FC

5296 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

Descripción / Description Internally inspect the FUSELAGE components: • Fuselage NOTE: During this inspection, the CPCP basic task skin panel at stringers, frames/bulkheads, and splices (SSI 53shall also be performed for this SSI. 30-07) Internally inspect the FUSELAGE components: • Fuselage machined bulkhead (SSI 53-30-30) NOTE: During this inspection, the CPCP basic task Internally inspect the FUSELAGE components: • Rear pressure bulkhead (SSI 53-30-36) shall also be performed for this SSI. Internally inspect the FUSELAGE components: • Fuselage machined bulkhead (SSI 53-30-30) Internally inspect the FUSELAGE components: • Fuselage to vertical stabilizer spar attachment fitting (SSI 53-30-38) Internally inspect the FUSELAGE components: • Bulkhead-to- NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. engine pylon attachment (SSI 53-30-35) Internally inspect the FUSELAGE components: • Frames (SSI 53-30-43) Externally inspect the FUSELAGE components: • Baggage door cutout structure (SSI 53-30-48) Externally inspect the FUSELAGE components: • Baggage door lateral L-shape (SSI 53-30-03) NOTE: During this inspection, the CPCP basic task Internally inspect the FUSELAGE components: • Rear pressure bulkhead (SSI 53-30-36) shall also be performed for this SSI. NOTE: During this inspection, the CPCP basic task Internally inspect the FUSELAGE components: • Baggage shall also be performed for this SSI. door cutout structure (SSI 53-30-48) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

Internally inspect the FUSELAGE components: Fuselage skin NOTE: During this inspection, the CPCP basic task panel at stringers, frames/bulkheads, and splices (SSI 53-30shall also be performed for this SSI. 07). Internally inspect the FUSELAGE components: Fuselage skin panel at stringers, frames/bulkheads, and splices (SSI 53-3007). Internally inspect the FUSELAGE components: Fuselage machined bulkhead (SSI 53-30-30). Internally inspect the FUSELAGE components: Fuselage machined bulkhead (SSI 53-30-30). Internally inspect the FUSELAGE components: Fuselage skin panel at pressure bulkhead (SSI 53-30-15). Internally inspect the FUSELAGE components: Fuselage to vertical stabilizer spar attachment fitting (SSI 53-30-38). Internally inspect the FUSELAGE components: • Bulkhead-toengine pylon attachment (SSI 53-30-35) Internally inspect the FUSELAGE components: • Bulkhead-toengine pylon attachment (SSI 53-30-35)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 10 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

53-31-00-220-843-A00

STRUCTURAL

DET

53-31-00-220-845-A00

STRUCTURAL

DET

53-31-00-220-C06-A00

CORROSION PROGRAM

DET

53-32-00-220-801-A00

STRUCTURAL

DET

-

53-32-00-220-802-A00

STRUCTURAL

DET

-

53-32-00-220-803-A00

STRUCTURAL

DET

-

53-32-00-220-804-A00

STRUCTURAL

DET

-

53-32-00-220-805-A00

STRUCTURAL

DET

-

53-32-00-220-806-A00

STRUCTURAL

DET

-

53-32-00-220-807-A00

STRUCTURAL

DET

-

Descripción / Description

Internally inspect the FUSELAGE components: • Baggage door cutout structure (SSI 53-30-48) Internally inspect the FUSELAGE components: • Fuselage skin longitudinal splice (SSI 53-30-08) Internally inspect the FUSELAGE components: • Toilet waste CPCP drain valve support (SSI 53-30-29) -

Internally inspect the FUSELAGE components: • Fuselage to vertical stabilizer spar attachment fitting (SSI 53-30-38) Internally inspect the FUSELAGE components: • Fuselage machined bulkhead (SSI 53-30-30) Internally inspect the FUSELAGE components: • Tail cone access door cutout structure (SSI 53-30-50) Externally inspect the FUSELAGE components: • L profile – Strake attachment (SSI 53-32-01) Internally inspect the FUSELAGE components: • Tail cone access door cutout structure (SSI 53-30-50) Internally inspect the FUSELAGE components: • Fuselage to vertical stabilizer spar attachment fitting (SSI 53-30-38) Internally inspect the FUSELAGE components: • Fuselage maquined bulkhead (SSI 53-30-30) Externally inspect the FUSELAGE components: • Tail cone access door cutout structure (SSI 53-30-50) Externally inspect the FUSELAGE components: • Tail cone access door cutout structure (SSI 53-30-50) External General Visual Inspection ZONES 191/192/193/194/195/196/197/198

53-32-00-220-808-A00

STRUCTURAL

DET

-

53-32-00-220-809-A00

STRUCTURAL

DET

-

53-Z191-213-002-A00

ZONAL

GVI

-

53-Z191-214-003-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 191/192/193/194/195/197/198 ACCESS 191ZB 192LB 193QL/RR/ AAB 194ER 195EL 197AB/CL/ DR 198CB

53-Z196-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONE 196. Access 196AL 196EL 196BR 196FR 196CZ 196DB 196GB

53-Z273-214-001-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 273/274. Access 273ATC 273BTC 273CTC.

54-50-00-220-801-A00

STRUCTURAL

DET

-

54-50-00-220-804-A00

STRUCTURAL

DET

-

54-50-00-220-805-A00

STRUCTURAL

DET

-

54-50-00-220-806-A00

STRUCTURAL

DET

-

54-50-00-220-807-A00

STRUCTURAL

DET

-

54-50-00-220-808-A01

STRUCTURAL

DET

-

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

Internally inspect the PYLON components: • Pylon spars I, II, III and IV (SSI 54-50-01) NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. Internally inspect the PYLON components: • Engine mounts including bolts (SSI 54-50-03). Externally inspect the PYLON components: • Pylon Skin (SSI 54-50-04) Internally inspect the PYLON components: • Pylon Skin (SSI 54-50-04) Internally inspect the PYLON components: • Pylon SPARS I,.II,. III and IV (SSI 54-50-01) Internally inspect the PYLON components: • AFT Engine Mounts including bolts (SSI 54-50-07) NOTE: Applicable to aircraft Post-Mod. SB 145-54-0011, and the flight cycles accumulated shall be based on the engine mount components.

NOTE: EWIS

VENTRAL FUEL TANK NOTE: EWIS REAR FUSELAGE (Applicable to Baggage compartment Class "D") (Not applicable Aerolitoral ERJ145 fleet)

Applicable to aircraft Pre Mod SB 145-54-0010 NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

Umbral Thrsld.

Intervalo Interval

19000 FC

4828 FC

-

4828 FC

-

30 MOS

EMB-135ER EMB-135LR

20000 FC

5000 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KLL

20000 FC

10000 FC

20000 FC

8193 FC

-

10000 FC

EMB-145XR

-

8193 FC

EMB-145XR

-

5000 FC

EMB-145XR

-

10000 FC

EMB-145XR

20000

10000 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

10000 FC

EMB-145XR

-

2C

EMB-145XR

-

2C

EMB-145XR

-

2C

EMB-145XR

-

2C

ALL

20000

5000 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

4000 FC

1000 FC

EMB-145XR

15000 FC

5000 FC

EMB-145XR

15000 FC

5000 FC

EMB-145XR

20000 FC

4115 FC

EMB-145XR

5000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB-135ER; EMB-135LR; EMB-135KE;F-GAC-01 EMB-135KL

5000

Efectividad Effect. EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 11 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

54-50-00-220-809-A00

STRUCTURAL

DET

-

54-50-00-220-809-A01

STRUCTURAL

DET

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

Applicable to aircraft Pre-Mod SB 145-54-10

4000 FC

1000 FC

EMB-145XR

Applicable to aircraft Post-Mod SB 145-54-10

5000 FC

5000 FC

EMB-145XR

30000

30000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

27345 FC

5257 FC

EMB-145XR

20000 FC

20000 FC

EMB-145XR

Descripción / Description Internally inspect the PYLON components: • AFT Engine Mounts including bolts (SSI 54-50-07) Internally inspect the PYLON components: • AFT Engine Mounts including bolts (SSI 54-50-07)

Internally inspect the PYLON components: • Pylon Yokes III and IV (SSI 54-50-02) NOTE: Applicable to aircraft Post-Mod. SB 145-54-0011.

54-50-00-220-810-A01

STRUCTURAL

DET

54-50-00-220-811-A00

STRUCTURAL

DET

-

54-50-00-230-801-A00

STRUCTURAL

SDE

-

Internally inspect the PYLON components: •Pylon Yokes III and IV (SSI 54-50-02) Internally inspect the PYLON components by Liquid Penetrate Inspection Method : •FWD Engine Mounts including bolts (SSI 54-50-03)

Applicable to aircraft Post-Mod SB 145-54-10

54-50-00-230-802-A00

STRUCTURAL

SDE

-

Internally inspect the PYLON components by Liquid Penetrant Inspection Method: • FWD Engine Mounts including bolts (SSI 54-50-03) NOTE: Applicable to aircraft Post-Mod. SB 145-54-0011, and the flight cycles accumulated shall be based on the engine mount c

54-50-00-250-801-A00

STRUCTURAL

SDE

-

Internally inspect the PYLON components by the Eddy Current method : •Pylon Yokes I and II (SSI 54-50-05)

27345 FC

20000 FC

EMB-145XR

54-50-00-250-803-A00

STRUCTURAL

SDE

-

Internally inspect the PYLON components by the Eddy Current method: • Pylon Yokes I and II upper flange (SSI 54-50-06)

27345 FC

5310 FC

EMB-145XR

30000

30000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

4227 FC

EMB-145ER; EMB-145EU; EMB-145EP

15000

15000 FC

EMB-145EP; EMB-145ER; EMB-145EU; EMB-145LR; EMB-145LU; EMB-145MK; EMB-145MP; EMB-145MR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

54-50-00-250-804-A00

STRUCTURAL

SDE

-

Internally inspect the PYLON components by the Eddy Current method: • Pylon Yokes I and II (SSI 54-50-05) NOTE: Applicable to aircraft Post-Mod. SB 145-54-0011.

55-10-00-220-806-A00

STRUCTURAL

DET

-

Internally inspect the HORIZONTAL STABILIZER components: • Skin splice at upper and lower surface (SSI 5510-16)

(*) NOTE: Applicable to aircraft Pre-Mod. SB 145-55Internally inspect the HORIZONTAL STABILIZER 0005, perform first inspection at 8000 FC, second components: • Front/Rear auxiliary spar center fitting ( SSI 55inspection at 12000 FC, and the subsequent every 10-19 ) 3A (Not applicable Aerolitoral fleet)

-

3A

EMB-145EU; EMB-145EP; EMB-145ER; EMB-135ER

Applicable to aircraft Pre-Mod SB 145-55-0005" (Not applicable Aerolitoral ERJ145 fleet)

55-10-00-220-807-A00

STRUCTURAL

DET

-

55-10-00-220-809-A00

STRUCTURAL

DET

-

Internally inspect the HORIZONTAL STABILIZER components: • Front spar center fittings ( SSI 55-10-20 )

(*) NOTE: Applicable to aircraft Pre-Mod. SB 145-550005, perform first inspection at 8000 FC, second inspection at 12000 FC, and the subsequent every 3A (Not Applicable Aerolitoral fleet)

-

3A

EMB-145EU; EMB-145EP; EMB-145ER

55-10-00-220-816-A00

STRUCTURAL

DET

-

Internally inspect the HORIZONTAL STABILIZER components: • Rear spar center fitting ( SSI 55-10-18 )

(*) NOTE: Applicable to aircraft Pre-Mod. SB 145-550005, perform first inspection at 8000 FC, second inspection at 12000 FC, and the subsequent every "3A" check

-

3A

EMB-145EU; EMB-145EP; EMB-145ER

55-10-00-220-818-A00

STRUCTURAL

DET

-

Externally inspect the HORIZONTAL STABILIZER components: • Skin from rib station YH=350 to rib YH=990 upper surfaces (SSI 55-10-02)

-

2599 FC

EMB-135LR; EMB-135ER; EMB-135KE; EMB-135KL F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 12 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

55-10-00-220-819-A00

STRUCTURAL

DET

-

-

3658 FC

EMB-135LR; EMB-135ER; EMB-135KE; EMB-135KL

55-10-00-220-820-A00

STRUCTURAL

DET

-

-

3658 FC

EMB-135LR; EMB-135ER; EMB-135KE; EMB-135KL

55-10-00-220-821-A00

STRUCTURAL

DET

-

Internally inspect the HORIZONTAL STABILIZER components: • From/Rear spar center fitting (SSI 55-10-19)

-

3658 FC

EMB-135LR; EMB-135ER; EMB-135KE; EMB-135KL

55-10-00-220-822-A00

STRUCTURAL

DET

-

Internally inspect the HORIZONTAL STABILIZER components: • From spar center fitting (SSI 55-10-20)

-

3658 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL; EMB-145XR

55-10-00-220-824-A00

STRUCTURAL

DET

-

-

10000 FC

EMB-145XR

55-10-00-220-825-A00

STRUCTURAL

DET

-

4000 FC

2532 FC

EMB-145XR

55-10-00-220-826-A00

STRUCTURAL

DET

-

-

2532 FC

EMB-145XR

55-10-00-220-827-A00

STRUCTURAL

DET

-

-

2532 FC

EMB-145XR

55-10-00-220-828-A00

STRUCTURAL

DET

-

-

2599 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

55-10-00-220-829-A00

STRUCTURAL

DET

-

-

2599 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

55-10-00-220-830-A00

STRUCTURAL

DET

-

-

10000 FC

EMB-145XR

55-10-00-220-832-A00

STRUCTURAL

DET

-

-

6226 FC

EMB-145XR

55-10-00-220-833-A00

STRUCTURAL

DET

-

-

2532 FC

EMB-145XR

55-10-00-220-834-A00

STRUCTURAL

DET

-

-

6226 FC

EMB-145XR

55-30-00-210-801-A00

STRUCTURAL

GVI

-

Internally inspect the VERTICAL STABILIZER components: • Rear spar actuator support fitting (elevator) (SSI 55-30-77)

20000 FC

10000 FC

55-30-00-210-804-A00

STRUCTURAL

GVI

-

Internally inspect the VERTICAL STABILIZER components: • PCU support fittings (SSI 55-30-80)

20000 FC

10000 FC

55-30-00-220-801-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-to-horizontal stabilizer attachment fitting to spar 3 (SSI 5530-50)

20000 FC

10000 FC

55-30-00-220-802-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Spar 1 - tip rib attachment (SSI 55-30-53)

20000 FC

10000 FC

55-30-00-220-803-A00

STRUCTURAL

DET

-

Externally inspect the VERTICAL STABILIZER components: • Rudder hinge fittings (SSI 55-30-78)

20000 FC

10000 FC

55-30-00-220-805-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fitting hinge support (SSI 55-30-76)

20000 FC

5574 FC

Descripción / Description Internally inspect the HORIZONTAL STABILIZER components: • Skin splice at upper and lower surface (SSI 5510-16) Internally inspect the HORIZONTAL STABILIZER components: • Rear spar center fitting (SSI 55-10-18)

Externally inspect the HORIZONTAL STABILIZER components: • Skin, from fin to sta. YH=350 - lower surface (SSI 55-10-06) Internally inspect the HORIZONTAL STABILIZER components: • Skin splice at upper and lower surface (SSI 5510-16) Internally inspect the HORIZONTAL STABILIZER components: • Rear spar center fitting (SSI 55-10-18) Internally inspect the HORIZONTAL STABILIZER components: •Front/Rear auxiliary spar center fitting (SSI 5510-19) Externally inspect the HORIZONTAL STABILIZER components: • Skin from fin to sta. YH=350-upper surface (SSI 55-10-01) Externally inspect the HORIZONTAL STABILIZER components: • Skin from fin to sta. YH=350-lower surface (SSI 55-10-06) Externally inspect the HORIZONTAL STABILIZER components: • Elevator support fittings (SSI 55-10-15) Externally inspect the HORIZONTAL STABILIZER components: • Skin, from rib sta YH=350 to rib YH=990 upper surface (SSI 55-10-02) Internally inspect the HORIZONTAL STABILIZER components: • Front Spar center fittings (SSI 55-10-20) Externally inspect the HORIZONTAL STABILIZER components: • Skin, from fin to sta. YH=350 upper surface (SSI 55-10-01)

EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135KE; EMB-135KL; EMB-135LR F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 13 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

55-30-00-220-806-A00

STRUCTURAL

DET

-

20000 FC

10000 FC

55-30-00-220-807-A00

STRUCTURAL

DET

-

20000 FC

10000 FC

55-30-00-220-814-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Tip rib (SSI 55-30-69)

20000 FC

10000 FC

55-30-00-220-815-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-to-horizontal stabilizer support actuators, including bolt (SSI 55-30-75)

20000 FC

10000 FC

55-30-00-220-816-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Actuator support fittings (rudder) (SSI 55-30-79)

20000 FC

10000 FC

55-30-00-220-823-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Spar 1 (web and cap), from fuselage contour line to tip rib (SSI 55-30-68)

-

10000 FC

EMB-145XR

55-30-00-220-824-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-to-fuselage attachment fitting to spar 3 (SSI 55-30-54)

-

8003 FC

EMB-145XR

55-30-00-220-825-A00

STRUCTURAL

DET

-

-

8003 FC

EMB-145XR

55-30-00-220-826-A00

STRUCTURAL

DET

-

-

8003 FC

EMB-145XR

55-30-00-220-827-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-to-fuselage attachment fitting to spar 2 (SSI 55-30-57)

-

8003 FC

EMB-145XR

55-30-00-220-828-A00

STRUCTURAL

DET

-

Internally inspect the VERTICAL STABILIZER components: • Fin-to-fuselage attachment fitting to spar 1 (SSI 55-30-87)

-

8003 FC

EMB-145XR

55-30-00-220-829-A00

STRUCTURAL

DET

-

-

8003 FC

EMB-145XR

55-30-00-220-830-A00

STRUCTURAL

DET

-

-

8003 FC

EMB-145XR

55-30-00-220-831-A00

STRUCTURAL

DET

-

-

8003 FC

EMB-145XR

55-30-00-220-832-A00

STRUCTURAL

DET

-

-

8003 FC

EMB-145XR

55-30-00-250-801-A00

STRUCTURAL

SDE

-

-

29600 FC

57-10-00-210-801-A00

STRUCTURAL

GVI

-

20000 FC

16000 FC

57-10-00-220-805-A00

STRUCTURAL

DET

-

20000 FC

5000 FC

57-10-00-220-818-A00

STRUCTURAL

DET

-

20000 FC

5852 FC

57-10-00-220-819-A00

STRUCTURAL

DET

-

-

5852 FC

Descripción / Description Internally inspect the VERTICAL STABILIZER components: • Fin-to-horizontal stabilizer attachment fitting to auxiliary spar 52% (SSI 55-30-51) Internally inspect the VERTICAL STABILIZER components: • Fin-to-horizontal stabilizer attachment fitting to auxiliary spar 41% (SSI 55-30-52)

Internally inspect the VERTICAL STABILIZER components: • Fin-to-fuselage attachment fitting to auxiliary spar 52% (SSI 5530-55) Internally inspect the VERTICAL STABILIZER components: • Fin-to-fuselage attachment fitting to auxiliary spar 41% (SSI 5530-55)

Internally inspect the VERTICAL STABILIZER components: • Fin-to-fuselage attachment fitting to bulkhead 77 (SSI 55-3059) Internally inspect the VERTICAL STABILIZER components: • Fin-to-fuselage attachment fitting to bulkhead 78 (SSI 55-3060) Internally inspect the VERTICAL STABILIZER components: • Fin-to-fuselage attachment fitting to bulkhead 79 (SSI 55-3061) Internally inspect the VERTICAL STABILIZER components: • Fin-to-fuselage attachment fitting to bulkhead 80 (SSI 55-3062) Externally inspect the VERTICAL STABILIZER components by the eddy current inspection method: • Fitting hinge support (SSI 55-30-76) Externally inspect the WING STUB components: • Spar 2 brackets and rib 2A web attachments (SSI 57-10-27) Internally inspect the WING STUB components: • Spar 2 brackets and rib 2A web attachments (SSI 57-10-27) Internally inspect the WING STUB components: • Spar 2 Lower skin attachments (SSI 57-10-06) Internally inspect the WING STUB components: • Spar 2 Auxiliary cap attachments and auxiliary cap splice at wing attachments (SSI 57-10-08)

Efectividad Effect. EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

EMB-145XR; EMB-135ER; EMB-135KE; EMB-135KL; EMB-135LR EMB-145XR; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135LR; EMB-135KE; EMB-135KL EMB-135LR; EMB-135KE; EMB-135KL EMB-135LR; EMB-135KE; EMB-135KL;F-GAC-01 EMB-145XR SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 14 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

57-10-00-220-820-A00

STRUCTURAL

DET

-

57-10-00-220-821-A00

STRUCTURAL

DET

-

57-10-00-220-823-A00

STRUCTURAL

DET

-

57-10-00-220-824-A00

STRUCTURAL

DET

-

57-10-00-220-825-A00

STRUCTURAL

DET

-

57-10-00-220-828-A00

STRUCTURAL

DET

-

57-10-00-220-829-A00

STRUCTURAL

DET

-

57-10-00-220-830-A00

STRUCTURAL

DET

-

57-10-00-220-831-A00

STRUCTURAL

DET

-

57-10-00-220-832-A00

STRUCTURAL

DET

-

57-10-00-250-801-A01

STRUCTURAL

SDE

-

57-11-00-220-805-A00

STRUCTURAL

DET

-

57-11-00-220-807-A00

STRUCTURAL

DET

-

57-11-00-220-809-A00

STRUCTURAL

DET

-

57-11-00-220-810-A00

STRUCTURAL

DET

-

57-11-00-220-811-A00

STRUCTURAL

DET

57-11-00-220-812-A00

STRUCTURAL

DET

57-11-00-220-813-A00

STRUCTURAL

DET

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

8000 FC

5000 FC

EMB-145XR

8000 FC

5091 FC

EMB-145XR

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

-

6596 FC

EMB-145XR

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

-

4271 FC

EMB-145XR

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

-

4271 FC

EMB-145XR

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

-

7144 FC

EMB-145XR

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

-

7144 FC

EMB-145XR

-

7144 FC

EMB-145XR

-

7144 FC

EMB-145XR

-

5091 FC

EMB-145XR

24000 FC

ALL

20000 FC

10000 FC

EMB-145XR

20000 FC

20000 FC

EMB-145XR; EMB-135LR; EMB-135KE; EMB-135KL

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

20000 FC

20000 FC

EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

20000 FC

10000 FC

EMB-145XR

-

Internally inspect the WING STUB components: • Spar 1 Titanium fitting attachments, fuselage bulkhead attachments at NOTE: During this inspection, the CPCP basic task frame 40, L - shape fuselage frame 40 attachments & fuselage shall also be performed for this SSI. stringers attachments (SSI 57-11-19)

20000 FC

5000 FC

EMB-135ER

-

Internally inspect the WING STUB components: • Spar 1 Titanium fitting attachments, fuselage bulkhead attachments at frame 40, L - shape fuselage frame 40 attachments & fuselage stringers attachments (SSI 57- 11-19)

20000 FC

10000 FC

EMB-145XR; EMB-135LR; EMB-135KE; EMB-135KL

-

Externally inspect the WING STUB components:• Spar 3 Fuselage bulkhead attachments at frame 50, L -shape fuselage frame 50 attachments & fuselage stringers attachments (SSI 57-11-21)

20000 FC

5000 FC

EMB-135ER

Descripción / Description Externally inspect the WING STUB components: • Spar 2 lower skin attachments (SSI 57-10-06) Internally inspect the WING STUB components: • Spar 2 Lower skin attachments (SSI 57-10-06) Externally inspect the WING STUB components: • Lower skinspanwise splice at spart 2, access holes, stringers, integral milled panels and spanwise splice of integral panel (SSI 57-1001) Externally inspect the WING STUB components: • Lower skinribs 1, 2 and 3 attachments and tire compartment wall attachments (SSI 57-10-02). Internally inspect the WING STUB components: • Lower skinribs 1, 2 and 3 attachments and tire compartment wall attachments (SSI 57-10-02). Externally inspect the WING STUB components: • Spar 1auxiliary cap attachments and auxiliary cap splice at wing attachments (SSI 57-10-05). Externally inspect the WING STUB components: • Spar 1lower skin attachments (SSI 57-10-03) Internally inspect the WING STUB components: • Spar 1 lower skin attachments (SSI 57-10-03) Internally inspect the WING STUB components: • Spar 1 Auxiliary Cap attachments and Auxiliary cap splice at wing attachments (SSI 57-10-05) Internally inspect the WING STUB components: • Spar 2 Auxiliary Cap attachments and Auxiliary cap splice at wing attachments (SSI 57-10-05) Externally inspect the WING STUB components using Eddy Current inspection method: • Rib 4 – lower flange and web (SSI 57-10-11) NOTE: Applicable to aircraft Post-Mod. SB 145-57-0047. Externally inspect the WING STUB components: • Fuselage bulkhead at frame 40 and its attachments to frame 40 (SSI 5711-23) Internally inspect the WING STUB components:• Lower skin rear fitting-to-skin attachments and spars 1 & 2 -stub-to-wing attachments (SSI 57-11-17) Externally inspect the WING STUB components: • Fuselage bulkhead at frame 50 and its attachments to frame 50 (SSI 5711-25) Internally inspect the WING STUB components: • Fuselage bulkhead attachments to frame 46 (SSI 57-11-24)

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 15 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

57-11-00-220-815-A00

STRUCTURAL

DET

-

57-11-00-220-816-A00

STRUCTURAL

DET

-

57-11-00-220-817-A00

STRUCTURAL

DET

-

57-11-00-220-818-A00

STRUCTURAL

DET

-

57-11-00-220-819-A00

STRUCTURAL

DET

-

57-11-00-220-820-A00

STRUCTURAL

DET

-

57-11-00-220-821-A00

STRUCTURAL

DET

-

57-11-00-220-822-A00

STRUCTURAL

DET

-

57-11-00-220-823-A00

STRUCTURAL

DET

-

57-11-00-220-824-A00

STRUCTURAL

DET

-

57-11-00-220-825-A00

STRUCTURAL

DET

-

57-11-00-220-826-A00

STRUCTURAL

DET

-

57-11-00-220-827-A00

STRUCTURAL

DET

-

57-11-00-220-828-A00

STRUCTURAL

DET

-

57-11-00-220-829-A00

STRUCTURAL

DET

-

57-11-00-220-830-A00

STRUCTURAL

DET

-

57-11-00-220-832-A00

STRUCTURAL

DET

-

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

20000 FC

20000 FC

EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

5000 FC

EMB-145XR; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

10000 FC

20000 FC

10000 FC

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

20000 FC

10000 FC

EMB-145XR

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

20000 FC

5000 FC

EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

10000 FC

EMB-145XR

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

20000 FC

5000 FC

EMB-135ER

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

20000 FC

10000 FC

EMB-145XR; EMB-135LR; EMB-135KE; EMB-135KL

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

20000 FC

5000 FC

EMB-145XR; EMB-135LR; EMB-135KE; EMB-135KL

Externally inspect the WING STUB components: • Spar 1 Titanium fitting attachments, fuselage bulkhead attachments at NOTE: During this inspection, the CPCP basic task frame 40, L - shape fuselage frame 40 attachments & fuselage shall also be performed for this SSI. stringers attachments (SSI 57-11-19).

20000 FC

5000 FC

EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

During this inspection, the CPCP basic task shall also be performed for this SSI.

20000 FC

5617 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

20000 FC

5000 FC

EMB-135ER

Internally inspect the WING STUB components: • Lower skin rear fitting-to-skin attachments and spars 1 & 2 -stub-to-wing NOTE: During this inspection, the CPCP basic task attachments (SSI 57-11-17) NOTE: During this inspection, the shall also be performed for this SSI. CPCP basic task shall also be performed for this SSI.

20000 FC

20000 FC

EMB-135ER

20000 FC

9388 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

5000 FC

EMB-145XR

20000 FC

9238 FC

EMB-145XR

Descripción / Description Internally inspect the WING STUB components: • Fuselage NOTE: During this inspection, the CPCP basic task bulkhead at frame 50 and its attachments to frame 50 (SSI 57shall also be performed for this SSI. 11-25) Internally inspect the WING STUB components: • Spar 2 Titanium fitting attachments and fuselage bulkhead at frame 46 (SSI 57-11-20) Externally inspect the WING STUB components: • Lower skin NOTE: During this inspection, the CPCP basic task rear fitting-to-skin attachments and spars 1 & 2 -stub-to-wing shall also be performed for this SSI. attachments(SSI 57-11-17) Externally inspect the WING STUB components: • Spar 3 and NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. rib 4 rod-end link (SSI 57-11-22) Externally inspect the WING STUB components: • Fuselage bulkhead attachments to frame 46 (SSI 57-11-24) Externally inspect the WING STUB components: • Spar 2 Titanium fitting attachments and fuselage bulkhead attachments at frame 46 (SSI 57-11-20) Internally inspect the WING STUB components: • Fuselage bulkhead at frame 40 and its attachments to frame 40 (SSI 5711-23) Internally inspect the WING STUB components: • Spar 3 Fuselage bulkhead attachments at frame 50, L -shape fuselage frame 50 attachments & fuselage stringers attachments (SSI 57-11-21) Internally inspect the WING STUB components: • Spar 3 Fuselage bulkhead attachments at frame 50, L -shape fuselage frame 50 attachments & fuselage stringers attachments (SSI 57-11-21) Externally inspect the WING STUB components: • Spar 3 Fuselage bulkhead attachments at frame 50, L -shape fuselage frame 50 attachments & fuselage stringers attachments (SSI 57-11-21)

Internally inspect the WING STUB components: • Spar 1 Lower front fitting attachments and spar 2 - lower rear fitting attachments (SSI 57-11-18) Internally inspect the WING STUB components: • Spar 2 Titanium fitting attachments and fuselage bulkhead at frame 46 (SSI 57-11-20)

Internally inspect the WING STUB components: • Fuselage NOTE: During this inspection, the CPCP basic task bulkhead at frame 40 and its attachments to frame 40 (SSI 57shall also be performed for this SSI. 11-23) Externally inspect the WING STUB components: • Lower skin rear fitting and integral rear fitting panel (SSI 57-11-15) Externally inspect the WING STUB components: • Spar 3 and NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI. rib 4 rod-end link (SSI 57-11-22).

EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB135KL

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 16 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Descripción / Description

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

57-11-00-220-833-A00

STRUCTURAL

DET

-

Externally inspect the WING STUB components: • Fuselage NOTE: During this inspection, the CPCP basic task bulkhead at frame 40 and its attachments to frame 40 (SSI 57shall also be performed for this SSI. 11-23).

20000 FC

9388 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-11-00-220-834-A00

STRUCTURAL

DET

-

Externally inspect the WING STUB components: • Fuselage bulkhead attachments to frame 46 (SSI 57-11-24).

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

20000 FC

9047 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-11-00-220-835-A00

STRUCTURAL

DET

-

Internally inspect the WING STUB components: • Fuselage bulkhead attachments to frame 46 (SSI 57-11-24).

NOTE: During this inspection, the CPCP basic task shall also be performed for this SSI.

20000 FC

9047 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-11-00-220-836-A00

STRUCTURAL

DET

-

20000 FC

10000 FC

EMB-145XR

57-11-00-220-837-A00

STRUCTURAL

DET

-

20000 FC

10000 FC

EMB-145XR

57-11-00-220-838-A00

STRUCTURAL

DET

-

20000 FC

5617 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-21-00-210-803-A00

STRUCTURAL

GVI

-

20000 FC

5000 FC

57-21-00-210-821-A00

STRUCTURAL

GVI

-

20000 FC

20000 FC

57-21-00-210-822-A00

STRUCTURAL

GVI

-

20000 FC

2500 FC

EMB-145XR

57-21-00-210-823-A00

STRUCTURAL

GVI

-

-

6420 FC

EMB-145XR

57-21-00-210-825-A00

STRUCTURAL

GVI

-

-

5000 FC

57-21-00-210-827-A00

STRUCTURAL

GVI

57-21-00-210-831-A00

STRUCTURAL

GVI

57-21-00-220-807-A00

STRUCTURAL

DET

57-21-00-220-808-A00

STRUCTURAL

DET

57-21-00-220-809-A00

STRUCTURAL

DET

57-21-00-220-810-A00

STRUCTURAL

DET

57-21-00-220-816-A00

STRUCTURAL

DET

57-21-00-220-817-A00

STRUCTURAL

DET

57-21-00-220-818-A00

STRUCTURAL

DET

57-21-00-220-820-A00 57-21-00-220-C01-A00 57-21-00-220-C02-A00 57-21-00-250-801-A00

STRUCTURAL CORROSION PROGRAM CORROSION PROGRAM STRUCTURAL

DET DET DET SDE

Externally inspect the WING STUB components: • Lower fitting NOTE: During this inspection, the CPCP basic task attachments and spar 2 lower rear fitting attachments (SSI 57shall also be performed for this SSI. 11-18) Internally inspect the WING STUB components • Spar 1 lower NOTE: During this inspection, the CPCP basic task front fitting attachments and spar 2 lower rear fitting shall also be performed for this SSI. attachments (SSI 57-11-18) Externally inspect the WING STUB components • Spar 1 lower NOTE: During this inspection, the CPCP basic task front fitting attachments and spar 2 lower rear fitting shall also be performed for this SSI. attachments (SSI 57-11-18) Internally inspect the WING components: • Lower skin/spar attachments (SSI 57-21-36) Internally inspect the WING components: Lower skin access holes (SSI 57-21-32) Externally inspect the WING components: Upper skin/spar attachments (SSI 57-21-37) Internally inspect the WING components: Lower skin panel spanwise joint (SSI 57-21-30) Internally inspect the WING components: • Skin panel (SSI 5721-26) Externally inspect the WING components: Skin panels (SSI 5721- 26) Internally inspect the WING components: • Lower skin access holes (SSI 57-21-32)

Internally inspect the WING components: • Lower skin/spar attachments (SSI 57-21-36) Externally inspect the WING components: • Lower skin/spar attachments (SSI 57-21-36) Internally inspect the WING components: • Upper skin/spar attachments (SSI 57-21-37) Externally inspect the WING components: • Skin panels (SSI 57-21-26) Externally Inspect the WING components: • Lower vent hole (SSI 57-21-33) Externally Inspect the WING components: • Actuator Access holes (SSI 57-21-34) Externally Inspect the WING components: • Lower Skin Access holes (SSI 57-21-32) Internally Inspect the WING components: • Lower skin/spar attachments (SSI 57-21-36) Externally Inspect the WING components: • Lower skin access CPCP holes (SSI 57-21-32) Externally Inspect the WING components: • Skin panels (SSI CPCP 57-21-26) Externally inspect the WING components by using Eddy Current method: Lower skin panel chordwise joint (SSI 57-2129) -

18298 FC

EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

EMB-145XR EMB-135LR; EMB-135KE; EMB-135KL; EMB-135ER EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000

20000 FC

20000 FC

3335 FC

EMB-145XR

-

3335 FC

EMB-145XR

20000 FC

5000 FC

EMB-145XR

20000 FC

2500 FC

EMB-145XR

-

3335 FC

EMB-145XR

-

3335 FC

EMB-145XR

-

3335 FC

EMB-145XR

20000 FC

8160 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

96 MOS

60 MOS

EMB-145XR

96 MOS

60 MOS

EMB-145XR

-

30000 FC

EMB-145XR F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 17 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

57-22-00-210-803-A00

STRUCTURAL

GVI

57-22-00-210-805-A00

STRUCTURAL

GVI

57-22-00-220-801-A00

STRUCTURAL

DET

57-22-00-220-806-A00

STRUCTURAL

DET

57-22-00-220-807-A00

STRUCTURAL

DET

57-22-00-220-C02-A00 57-22-00-220-C03-A00

CORROSION PROGRAM CORROSION PROGRAM

DET DET

57-23-00-210-802-A00

STRUCTURAL

GVI

57-23-00-210-803-A00

STRUCTURAL

GVI

57-23-00-210-804-A00

STRUCTURAL

GVI

Cat. Cat.

Descripción / Description

Internally inspect the WING components: • Spar 1 cap (SSI 5722-41) Internally inspect the WING components: • Spar 1 cap (SSI 5722-41) Externally inspect the WING components: • Spar 1/web and stiffeners (SSI 57-22-40) Externally inspect the WING components: Spar 1/web and stiffeners (SSI 57-22-40 Internally inspect the WING components: • Spar 1/Leading edge attachments (SSI 57-22-43) Internally inspect the WINGLET components: • Front spar CPCP attachment points (SSI 57-22-46) Internally inspect the WING components: • Spar 1, web and CPCP stiffeners (SSI 57-22-40) Internally inspect the WING components: • Spar 2 cap (SSI 5723-46) Internally inspect the WING components: • Spar 2 cap (SSI 5723-46) Internally inspect the WING components: • Spar 2 cap (SSI 5723-46) -

Umbral Thrsld.

Intervalo Interval

20000 FC

10000 FC

EMB-145XR

20000 FC

8736 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

10000 FC

EMB-145XR

20000 FC

10000 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

10000 FC

EMB-145XR

-

60 MOS

-

30 MOS

20000 FC

10000 FC

20000 FC

10000 FC

20000 FC

10000 FC

Efectividad Effect.

EMB-145XR EMB-135ER EMB-135LR EMB-135KE EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR EMB-145XR EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-23-00-220-801-A00

STRUCTURAL

DET

-

Internally inspect the WING components: • Spar 2/web and stiffeners (SSI 57-23-45)

20000 FC

10000 FC

57-23-00-220-804-A00

STRUCTURAL

DET

-

Internally inspect the WING components: • Spar 2/web cutouts (SSI 57-23-47)

20000 FC

10000 FC

57-23-00-220-C02-A00

CORROSION PROGRAM

DET

CPCP

Internally inspect the WINGLET components: • Rear spar attachment points (SSI 57-23-50)

-

60 MOS

EMB-145XR

20000 FC

5000 FC

EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

60 MOS

EMB-145XR

-

120 MOS

EMB-145XR

96 MOS

60 MOS

EMB-145XR

500 FC

EMB-145EU; EMB-145EP; EMB-145ER; EMB-135ER

-

2500 FC

EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

16459 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

10413 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

20000 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-24-00-210-801-A00 57-25-00-220-C01-A00 57-25-00-220-C02-A00 57-25-00-220-C03-A00 57-26-00-220-802-A00

STRUCTURAL CORROSION PROGRAM CORROSION PROGRAM CORROSION PROGRAM STRUCTURAL

GVI

-

DET

CPCP

DET DET DET

Internally inspect the WING components: • Spar 3 cap (SSI 5724-50)

Internally inspect the WINGLET components: • Rib 25 (SSI 5725-57) Internally inspect the WING components: • Rib main box (SSI CPCP 57-25-53) Internally inspect the WING components: • Lower skin/rib CPCP attachment x (SSI 57-25-54) Externally inspect the WING components: • FWD & AFT side brace fittings - MLG (SSI 57-26-56)

57-26-00-220-802-A01

STRUCTURAL

DET

-

Externally inspect the WING components: • FWD & AFT side brace fittings - MLG (SSI 57-26-56)

57-26-00-250-804-A00

STRUCTURAL

SDE

-

Externally inspect the WING components using Eddy Current Inspection Method: • Aft upper trunnion (SSI 57-26-95)

57-26-00-250-804-A01

STRUCTURAL

SDE

-

Externally inspect the WING components using Eddy Current Inspection Method: • Aft upper trunnion (SSI 57-26-95) P/N: 145-67014-011/012

57-26-00-250-804-A02

STRUCTURAL

SDE

-

Externally inspect the WING components using Eddy Current Inspection Method: • Aft upper trunnion (SSI 57-26-95) P/N: 145-67014-009/010/013/014

Applicable to A/C Pre-Mod. SB 145-57-0009.

Applicable to aircraft Pre-Mod. SB 145-57-0018.

Applicable only to Aft Upper Trunnion P/N: 14567014-001/002/003/004/005/006/007/ 008 (Record LH P/N Installed:__________) (Record RH P/N Installed:__________) Applicable only to Aft Upper Trunnion P/N: 14567014-011/012 (Record LH P/N Installed:__________) (Record RH P/N Installed:__________) Applicable only to trunnion P/N: 145-67014009/010/013/014 (Record LH P/N Installed:__________) (Record RH P/N Installed:__________)

-

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Código: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 15 -1- 18 .

SECCIÓN 15. TARES NO APLICABLES "NOT APPLICABLE TASKS" Número de Tarea Task Number

Grupo Group

Tipo Type

Cat. Cat.

Umbral Thrsld.

Intervalo Interval

Efectividad Effect.

57-26-00-250-805-A00

STRUCTURAL

SDE

-

Externally inspect the WIING components using Eddy Current Inspection Method: • Fwd upper Trunnion (SSI 57-26-96)

20000 FC

20000 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-26-00-250-806-A00

STRUCTURAL

SDE

-

Externally inspect the WIING components using Eddy Current Inspection Method: • Lower bearing cap (SSI 57-26-94)

-

22921 FC

EMB-145XR

57-26-00-250-807-A00

STRUCTURAL

SDE

-

Externally inspect the WIING components using Eddy Current Inspection Method: • Aft upper Trunnion (SSI 57-26-95)

-

30000 FC

EMB-145XR

57-26-00-250-810-A00

STRUCTURAL

SDE

-

Externally inspect the WING components using Eddy Current Inspection Method: • Lower Bearing Cap (SSI 57-26-94)

-

30000 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

57-26-00-250-811-A00

STRUCTURAL

SDE

-

Externally inspect the WING components using Eddy Current Inspection Method: • Forward Upper Trunnion (SSI 57-26-96)

-

22921 FC

EMB-145XR

57-28-00-210-810-A00

STRUCTURAL

GVI

-

-

10000 FC

EMB-145XR

-

3746 FC

EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

7229 FC

57-28-00-210-812-A00

STRUCTURAL

GVI

-

57-28-00-210-814-A00

STRUCTURAL

GVI

-

Descripción / Description

Internally inspect the WING components: • Lower skin, torque box (SSI 57-28-58) Externally inspect the WING components: •Attachment lugs aileron (SSI 57-28-66) Externally inspect the WING components: • Ribs, torque box (SSI 57-28-60)

57-28-00-220-804-A00

STRUCTURAL

DET

-

Internally inspect the WING components: • Spar attachment torque box (SSI 57-28-57)

57-28-00-220-807-A00

STRUCTURAL

DET

-

Externally inspect the WING components: • Center track and rib15 trailing edge (SSI 57-28-69)

57-28-00-220-809-A00

STRUCTURAL

DET

-

57-28-00-220-810-A00

STRUCTURAL

DET

-

57-28-00-220-811-A00

STRUCTURAL

DET

-

57-28-00-220-812-A00

STRUCTURAL

DET

-

Applicable to A/C Pre-Mod SB 145-57-0008 (Not Applicable all Aerolitoral EJ145fleet)

Externally inspect the WING components: • Center track and rib15 trailing edge (SSI 57-28-69) Externally inspect the WING components: • Upper skin, Torque box (SSI 57-28-61) Externally inspect the WING components: • Attachment center flap outboard track (SSI 57-28-68) Externally inspect the WING components: • lower skin, torque box (SSI 57-28-58) Externally inspect the AILERON components: Hinge attachment, aileron (SSI 57-61-89) Internally Inspect the AILERON components: -Actuator attachment, aileron (SSI 57-61-90)

57-61-00-210-801-A00

STRUCTURAL

GVI

-

57-61-00-220-806-A00

STRUCTURAL

DET

-

57-Z551-213-002-A00

ZONAL

GVI

-

External General Visual Inspection ZONES 551/651/561/661

57-Z551-214-002-A00

ZONAL

GVI

-

Internal General Visual Inspection ZONES 551/651/561/661. Access 551AB 551BB 551CB 551DB 551EB 551FT 551GB 651AB 651BB 651CB 651DB 651EB 651FT 651GB 561AL 561BB 561CL 551DL 661AR 661BB 661CR 651DR

79-34-00-212-001-A01

SYSTEMS

GVI

6

Inspect Multi-Function Display for ENG1(2) OIL DEBRIS Maintenance Message (Applicable to aircraft equipped with AE3007 A1E Engine only)

EMB-145XR EMB-145XR; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-145EU; EMB-145EP; EMB-145ER; EMB-145LR; EMB-145LU; EMB-145MR; EMB-145MP; EMB-145MK; EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

20000 FC

20000 FC

-

2000 FC

-

3275 FC

EMB-145XR

-

5445 FC

EMB-145XR

-

3912 FC

EMB-145XR

-

5000 FC

EMB-145XR EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL EMB-135ER; EMB-135LR; EMB-135KE; EMB-135KL

-

3622 FC

-

5738 FC

WING

-

2C

EMB-145XR

WING NOTE: EWIS

-

2C

EMB-145XR

-

70 FH

EMB-145XR

F-GAC-01 SEP-07

Programa de Mantenimiento EMB-145

Codigo: M-PME-01

EMB 145 Maintenance Program

Revisión: 2 Fecha de Efectividad: 05-Abr-10 Page: 16 -1-1

SECCIÓN 16. TAREAS INTERNAS

LISTA DE TAREAS A continuación se presenta un listado de tareas (Job Card) y tareas de AMM utilizadas en el Mantenimiento de Las aeronaves EMBRAER ERJ-145 desarrolladas por Aerolitoral.

JOB CARD

DESCRIPTION

JC256007ALE

Verify and Inventory of Emergency Equipment

JC237001ALE

Voice Cockpit Recorder Reading

JC282101ALE 313102ALE 145

Electrcal Fuel Pumps Inspection Removal and installation of auxiliary flight data acquisition and management unit (AFDAMU) PCMCIA Card

34-61-00-470-801-A

FMS navigation data base (AMM task)

34-62-00-400-801-A

Dual fms navigation data base (AMM task)

34-62-00-400-802-A

Single fms navigation data (AMM task)

49-64-03-970-001-A00

Data readout from APU FADEC (AMM task)

A continuación se Anexan los formato de las tareas internas (Job Card) utilizados en el Mantenimiento de las aeronaves EMBRAER ERJ-145

F-GAC-01 SEP-07

TALLER DGAC No. 122

CLAVE F-GIN-23

Job Card EMERGENCY

REPAIR STATION NO. LVQY318F

Code

REVISIÓN

EMERGENCY EQUIPMMENT

Rev 3

Revision

FECHA DE EMISIÓN 01-Ago-08

INTERVALO

H–H

Interval

Hrs-Men

45 Days

1

ZONA

PANEL DE ACCESO

N° DE TAREA:

TAREA REEMPLAZADA

Zone

Access Panel (s)

Task number

Replaced Task

Issue Date

VERIFY AND INVENTORY OF EMERGENCY EQUIPMENT

200

JC256007ALE R3

FECHA DE REVISIÓN 15-JUN-09 Revision Date

N/A

INSTRUCTIONS: 1.- Verify the emergency equipment according with the LOPA (It´s into the pax cabin). 2.- Verify emergency equipment by condition. 3.- Verify emergency equipment by expiration date (when applicable). It is necessary that the either of expiration date are major to 2 months, in case that the expiration date are minor replace the component or if don’t exist material for replace, make a discrepancy including part number, serial number, and expiration date. 4.- Verify the F-GIN-19 Internal Tag Control, are in good conditions (Figure 1). If it is found damaged, notify to Inspector in order to replace it. 5.- Verify the correct installation of equipment, if a discrepancy is found, repair or locate as necessary.

Registration:

COMPONENT

VERIFY

PORTABLE FIRE EXTINGUISHER PORTABLE FIRE EXTINGUISHER PORTABLE FIRE EXTINGUISHER PBE PBE PBE FIRST AID KIT (5 EA) SEAT BELT EXTENSION LIVE VEST (OBSERVER) LIVE VEST (ATTENDANT) LIVE VEST (PILOT) LIVE VEST (PILOT) PORTABLE OXYGEN CYLINDER (WITH MASK)

EFFECTIVITY: ERJ-145 OF AEROLITORAL SERIES: ALL

JC256007ALE Page 1 of 3 01 Aug, 2008

TALLER DGAC No. 122

CLAVE F-GIN-23

Job Card EMERGENCY

REPAIR STATION NO. LVQY318F

Code

REVISIÓN

EMERGENCY EQUIPMMENT

Rev 3

Revision

FECHA DE EMISIÓN 01-Ago-08

INTERVALO

H–H

Interval

Hrs-Men

45 Days

1

ZONA

PANEL DE ACCESO

N° DE TAREA:

TAREA REEMPLAZADA

Zone

Access Panel (s)

Task number

Replaced Task

VERIFY AND INVENTORY OF EMERGENCY EQUIPMENT

200

JC256007ALE R3

Issue Date

FECHA DE REVISIÓN 15-JUN-09 Revision Date

N/A

PORTABLE OXYGEN CYLINDER (WITH MASK) RECHARGABLE FLASHLIGHT (4EA) AXE FLIGHT CREW EMERGENCY ROPE (2EA) SMOKE GOGGLE (3EA) DEMONSTARTION KIT (1EA) OXYGEN MASK (OBSERVER) OXYGEN MASK (CREW) OXYGEN MASK (CREW) OXYGEN CYLINDER EMERGENCY LOCATOR TRANSMITTER & BATTERY BUILT-IN-FIRE EXTINGUISHER LIVE VEST (ALL PASSENGERS)

Deliver this Job Card to Planning and Control Department. Figure 1

Through carrying out this Job Card, gives effect to the following tasks, as applied according to counties in the MRB for each of them, and P/N of the components installed:

EFFECTIVITY: ERJ-145 OF AEROLITORAL SERIES: ALL

JC256007ALE Page 2 of 3 01 Aug, 2008

TALLER DGAC No. 122

CLAVE F-GIN-23

Job Card EMERGENCY

REPAIR STATION NO. LVQY318F

Code

REVISIÓN

EMERGENCY EQUIPMMENT

Rev 3

Revision

FECHA DE EMISIÓN 01-Ago-08

INTERVALO

H–H

Interval

Hrs-Men

45 Days

1

ZONA

PANEL DE ACCESO

N° DE TAREA:

TAREA REEMPLAZADA

Zone

Access Panel (s)

Task number

Replaced Task

VERIFY AND INVENTORY OF EMERGENCY EQUIPMENT

200

25-60-00-212-001-A00 25-60-02-900-001-A03 26-24-01-720-001-A00

JC256007ALE R3

25-60-02-900-001-A00 25-60-02-900-001-A04 26-24-01-720-001-A01

Issue Date

FECHA DE REVISIÓN 15-JUN-09 Revision Date

N/A

25-60-02-900-001-A01 26-24-00-211-001-A00

25-60-02-900-001-A02 26-24-00-280-001-A00

Inspections had been performed satisfactorily by Aerolitoral Authorized Personnel, who certified that all jobs had been performed in accordance with Maintenance Program approved by National Authority (DGAC). Name Date

Lic. Num. Station

EFFECTIVITY: ERJ-145 OF AEROLITORAL SERIES: ALL

Signature

JC256007ALE Page 3 of 3 01 Aug, 2008

Ultrasonic TALLER DGAC No. 122

CLAVE F-GIN-23

Job Card

REPAIR STATION NO. LVQY318F

Code

Electrical Fuel Pump Inspection INTERVALO Interval Follow MIE145-28-001R2

155-157

192BR,192AL(only MP/ER´s) 155DZ,156DZ (only LR/LU´s)

Access Panel (s)

R1

Issue Date March 16, 2006

Fuel System.

1.50 PANEL DE ACCESO

Zone

Revision

FECHA DE EMISIÓN 04-19-06

H–H

Hrs-Men

ZONA

REVISIÓN

FECHA DE REVISIÓN

Revision Date September 17, 2008

N° DE TAREA:

TAREA REEMPLAZADA

Task number

JC282101ALER2

Replaced Task

JC282101ALER1

General: This task gives the procedure to inspect the electrical connectors of the fuel pump on aircraft, in order to comply with requirements from “FAA AD 2005-13-22 and BAD 2000-08-01R”, as outlined in MIE 145-28-001R2.

AIRCRAFT TAIL

S/N

Previous the Engineering Order accomplishment, verify: Required tools are available. Required Equipment are available. Material and/or components are available.

Technical Licensed No, Signature

Inspector Stamp

A. Make sure that the aircraft is safe for maintenance. B. On the circuit breaker panel, open the Fuel Pumps-1A,1B,1C(2A,2B,2C) circuit breakers and attach a DO-NOT-CLOSE red tag F-ING-06 C. Removed access panels 192BR, 192AL applicable to MP/EP Models; if the A/C is model LR/LU removed access panels 155DZ, 156DZ to get access to electrical connectors. D. Disconnect the fuel pump electrical connectors from mating aircraft connectors, cutting thermofit to have a better evaluation E. Perform a visual inspection for general condition on electrical connectors of the electrical fuel pump. Refer to fig 1 sheet 01 of 03 or sheet 02 of 03 taking account A/C model. 1) If there is any evidence of corrosion, such as surface irregularities or visual damage to the surface plating, and /or, if one or more pins are blackened, and/or if the connector elastomeric insert (surface material surrounding pins) has visible cracks or evidence of erosion or charring(blackened or burnt surface proceed as follows see figure 1 sheet 03 of 03: i) Replace damaged electric fuel pump P/N 2C7-4 with another one bearing the same Part Number. Refer to the applicable AMM Chapter 28-21-01 (TASK28-21-01-000-801-A or TASK 28-21-01-000-802-A for removal and TASK28-21-01-400-801-A or Task 28-21-01-400-802-A for installation, as applicable)- Fuel

EFFECTIVITY: EMBRAER 145 060,065,083,089,090,203,240,313,322,337,400,406,420,426,434,440,444,456,475,498 510,559,564,570,574,580,588,601,795,798,00803,00852,008601

JC282101ALER2

Page 1 of 6 SEPTEMBER 17 ,2008

Ultrasonic TALLER DGAC No. 122

CLAVE F-GIN-23

Job Card

REPAIR STATION NO. LVQY318F

Code

Electrical Fuel Pump Inspection INTERVALO Interval Follow

PANEL DE ACCESO

155-157

192BR,192AL(only MP/ER´s) 155DZ,156DZ (only LR/LU´s)

Zone

Access Panel (s)

R1

Issue Date March 16, 2006

Fuel System.

1.50

ZONA

Revision

FECHA DE EMISIÓN 04-19-06

H–H

Hrs-Men

MIE145-28-001R2

REVISIÓN

FECHA DE REVISIÓN

Revision Date September 17, 2008

N° DE TAREA: Task number

JC282101ALER2

TAREA REEMPLAZADA Replaced Task

Continuation….

JC282101ALER1 Technical Licensed No, Signature

Inspector Stamp

ii). Perform a visual inspection on the mating aircraft connectors: -

If there are signs of damage, replace affected mating aircraft connector P/N MS3476L14-4S with new ones bearing, the same P/N according to the instructions of Wiring Manual- Chapters 20-00-03 and 20-50-01Standard Practices- Airframe and 91-10-02-Vendor List. For electrical interconnections, see Wiring Manual-Chapter 28-21-50 or 28-21-51 as applicable-Fuel

-

If there are no signs of damage, replace only socket contacts P/N M39029/25-118 with new ones bearing, the same P/N according to instructions of the Wiring Manual-Chapters 20-00-03 and 20-50-01Standard Practices Airframe and 91-10-02-Vendor list.

F. If no discrepancy is found, apply the anti-corrosive spray P/N MIL-L-8177A TYPE I, GRADE B) to the electric connectors. The product must cover the contacts without excess of spray. G. Cover the connector with thermo restringent boot, covering cannon. Refer to AMM 28-21-01-401. Warning: Obey the safety precautions given in WM 20-10-00 to use the heating gun. Explosions can occur if you use the heating gun incorrectly near flammable material or fluid vents. H. Connect the electric connector. If applicable, heat the thermo restringent boot with a heating gun or similar equipment. Refer toAMM 28-21-01/401 I. Reinstall the fuel pump electrical connectors to the matting aircraft connectors. J. Restore the aircraft to normal reordering the task performed in accordance with MIE145-28-001R1

Reason of revision R1: Aircraft serial numbers added per aircraft incorporation, EFFECTIVITY: EMBRAER 145 060,065,083,089,090,203,240,313,322,337,400,406,420,426,434,440,444,456,475,498 510,559,564,570,574,580,588,601,795,798,00803,00852,008601

JC282101ALER2

Page 2 of 6 SEPTEMBER 17 ,2008

Ultrasonic TALLER DGAC No. 122

Job Card

REPAIR STATION NO. LVQY318F

Electrical Fuel Pump Inspection INTERVALO Interval Follow MIE145-28-001R2

Code

REVISIÓN Revision

R1

FECHA DE EMISIÓN 04-19-06

H–H

Hrs-Men

Fuel System.

1.50

Issue Date March 16, 2006

FECHA DE REVISIÓN

Revision Date September 17, 2008

ZONA

PANEL DE ACCESO

155-157

192BR,192AL(only MP/ER´s) 155DZ,156DZ (only LR/LU´s)

Zone

CLAVE F-GIN-23

N° DE TAREA:

Access Panel (s)

Task number

JC282101ALER2

TAREA REEMPLAZADA Replaced Task

JC282101ALER1

R2: Aircraft serial numbers added per new aircraft incorporation to the fleet. item G, description revised to to clarify how cannon nut shall be covered with thermo fit.

APPLICABLE TO EMB-145 LR/LU

FIGURE 1: INSPECTION ON THE ELECTRICAL CONNECTORS OF THE ELECTRIC FUEL PUMP EFFECTIVITY: EMBRAER 145 060,065,083,089,090,203,240,313,322,337,400,406,420,426,434,440,444,456,475,498 510,559,564,570,574,580,588,601,795,798,00803,00852,008601

JC282101ALER2

Page 3 of 6 SEPTEMBER 17 ,2008

Ultrasonic TALLER DGAC No. 122

Job Card

REPAIR STATION NO. LVQY318F

Electrical Fuel Pump Inspection INTERVALO Interval Follow MIE145-28-001R2

Fuel System.

1.50 PANEL DE ACCESO

155-157

192BR,192AL(only MP/ER´s) 155DZ,156DZ (only LR/LU´s)

Zone

Access Panel (s)

Code

REVISIÓN Revision

R1

FECHA DE EMISIÓN 04-19-06

H–H

Hrs-Men

ZONA

CLAVE F-GIN-23

Issue Date March 16, 2006

FECHA DE REVISIÓN

Revision Date September 17, 2008

N° DE TAREA: Task number

JC282101ALER2

TAREA REEMPLAZADA Replaced Task

JC282101ALER1

(SHEET 01 OF 03)

APPLICABLE TO EMB-145 MP/EP FIGURE 1: INSPECTION ON THE ELECTRICAL CONNECTORS OF THE ELECTRIC FUEL PUMP EFFECTIVITY: EMBRAER 145 060,065,083,089,090,203,240,313,322,337,400,406,420,426,434,440,444,456,475,498 510,559,564,570,574,580,588,601,795,798,00803,00852,008601

JC282101ALER2

Page 4 of 6 SEPTEMBER 17 ,2008

Ultrasonic TALLER DGAC No. 122

Job Card

REPAIR STATION NO. LVQY318F

Electrical Fuel Pump Inspection INTERVALO Interval Follow MIE145-28-001R2

Fuel System.

1.50 PANEL DE ACCESO

155-157

192BR,192AL(only MP/ER´s) 155DZ,156DZ (only LR/LU´s)

Zone

Access Panel (s)

Code

REVISIÓN Revision

R1

FECHA DE EMISIÓN 04-19-06

H–H

Hrs-Men

ZONA

CLAVE F-GIN-23

Issue Date March 16, 2006

FECHA DE REVISIÓN

Revision Date September 17, 2008

N° DE TAREA: Task number

JC282101ALER2

TAREA REEMPLAZADA Replaced Task

JC282101ALER1

(SHEET 02 OF 03)

FIGURE 1: INSPECTION ON THE ELECTRICAL CONNECTORS OF THE ELECTRIC FUEL PUMP EFFECTIVITY: EMBRAER 145 060,065,083,089,090,203,240,313,322,337,400,406,420,426,434,440,444,456,475,498 510,559,564,570,574,580,588,601,795,798,00803,00852,008601

JC282101ALER2

Page 5 of 6 SEPTEMBER 17 ,2008

Ultrasonic TALLER DGAC No. 122

Job Card

REPAIR STATION NO. LVQY318F

Electrical Fuel Pump Inspection INTERVALO Interval Follow MIE145-28-001R2

Fuel System.

1.50 PANEL DE ACCESO

155-157

192BR,192AL(only MP/ER´s) 155DZ,156DZ (only LR/LU´s)

Zone

Access Panel (s)

Code

REVISIÓN Revision

R1

FECHA DE EMISIÓN 04-19-06

H–H

Hrs-Men

ZONA

CLAVE F-GIN-23

Issue Date March 16, 2006

FECHA DE REVISIÓN

Revision Date September 17, 2008

N° DE TAREA: Task number

JC282101ALER2

TAREA REEMPLAZADA Replaced Task

JC282101ALER1

(SHEET 03 OF 03)

EFFECTIVITY: EMBRAER 145 060,065,083,089,090,203,240,313,322,337,400,406,420,426,434,440,444,456,475,498 510,559,564,570,574,580,588,601,795,798,00803,00852,008601

JC282101ALER2

Page 6 of 6 SEPTEMBER 17 ,2008

Job Card

CLAVE:

F-GIN-23

NÚMERO DE REVISIÓN:

1

FECHA DE REVISIÓN:

10-MAR-08

Code:

RECORDING

Revision:

Indicating and Recording System

Revision Date:

H – H:

INTERVALO: Interval:

Hrs-Men:

150 Hours

0.30

Removal and Installation of Auxiliary Flight Data Acquisition and Management Unit (AFDAMU) PCMCIA Card No. DE ORDEN DE INGENIERÍA:

No. DE TAREA:

313102ALE 145

Task Number :

Enginnering Order Number:

ZONA:

PANEL DE ACCESO:

Zone:

Access Panel (s):

272

272DR

REQUERIDO POR: Required by:

N/A

AEROLITORAL

AD:

SB:

This task apply to: A/C Registration:______________

Aircraft

Date:

______________

P/N: ______________________ S/N: ______________________ Position:_____________

Component

1. General This task gives the procedure to remove and install the AFDAMU PCMCIA Card and advise to Security Department that it was removed of A/C Registration. NOTE: This task just apply to A/Cs with the OIE145-31-002 and Task 313101ALE “Installation of Auxiliary Flight Data Acquisition and Management Unit (AFDAMU) P/N ED35E109-04-00” incorporated. A. Material, Equipment and Tools. •

KIT’s: None

•

Material: None

•

Consumables NEW P/N

DESCRIPTION

SG9PC1GSMB4I

PCMCIA FLASH MEMORY CARD 1 GB (Industrial ATA PC Card)

MC083

Masking tape (1 inch)

•

QTY RQD

DISP/ Notes

01

The PCMCIA CARD removed of AFDAMU MUST BE SENT TO MTY WAREHOUSE

2.5 in

Equipment and Tools: ITEM P/N

GSE 036 (AGE-00919-401) EFECTIVIDAD:

DESCRIPTION

Hydraulic Platform or Equivalent Platform or Stair

All EMB-145 Model

Effectivity

SERIAL A/C Registration (Serial Number)

XA-LLI (145060), XA-MLI (145065), XA-NLI (145083), XA-OLI (145089), XA-PLI (145090), XA-GLI (145203), XA-KAC (145322), XA-HLI (145337), XA-YLI (145400), XA-ZLI (145420), XA-WLI (145434), XA-FLI (145444), XA-JLI (145440), XA-KLI (145426), XA-XLI (145456), XA-RLI (145559), XA-ILI (145564), XA-ULI (145570), XA-VLI (145574), XA-SLI (145580), XA-QLI (145588), XA-TLI (145601), XA-ALI (145795), XA-BLI (145798), XA-CLI (14500803), XA-DLI (14500852), XA-ELI (14500861)

QTY RQD

01

313102ALE 145

Rev. 1 June 19th, 2008 Page 1 de 6

Job Card

CLAVE:

F-GIN-23

NÚMERO DE REVISIÓN:

1

FECHA DE REVISIÓN:

10-MAR-08

Code:

RECORDING

Revision:

Indicating and Recording System

Revision Date:

H – H:

INTERVALO: Interval:

Hrs-Men:

150 Hours

0.30

Removal and Installation of Auxiliary Flight Data Acquisition and Management Unit (AFDAMU) PCMCIA Card No. DE ORDEN DE INGENIERÍA:

No. DE TAREA:

313102ALE 145

Task Number :

Enginnering Order Number:

N/A

ZONA:

PANEL DE ACCESO:

Zone:

Access Panel (s):

272

272DR

REQUERIDO POR: Required by:

AEROLITORAL

AD:

SB:

This task apply to: A/C Registration:______________

Aircraft

Date:

______________

P/N: ______________________ S/N: ______________________ Position:_____________

Component

2. Procedure The steps below outline the general accomplishment instructions.

DESCRIPTION

Tech. Cert. No. Signature

Insp. Stamp

A. Make sure that the aircraft is safe for maintenance. B. Energize the aircraft with the External DC Power Supply (TASK 20-40-01-860-801-A). C. Make at the cockpit, on the circuit breaker panel, that the FDAU circuit breaker is closed, see Figure No. 1. D. Put up the hydraulic platform (GSE 036) or equivalent platform or Stair at the necessary height. E. Open the 272DR to get access to the aft avionics compartment (AMM 06-41-01/101). F. AFDAMU PCMCIA Card – Removal, see Figure No. 2 (a) On the AFDAMU (1) front panel, push down the lock release switch (7) to unlock the AFDAMU access door (6) and open it. (b) Push the release button (3) to eject the AFDAMU PCMCIA card (2) from the AFDAMU PCMCIA card slot (4). (c) Remove the AFDAMU PCMCIA card (2) from the AFDAMU PCMCIA card slot (4). EFECTIVIDAD:

All EMB-145 Model

Effectivity

SERIAL A/C Registration (Serial Number)

XA-LLI (145060), XA-MLI (145065), XA-NLI (145083), XA-OLI (145089), XA-PLI (145090), XA-GLI (145203), XA-KAC (145322), XA-HLI (145337), XA-YLI (145400), XA-ZLI (145420), XA-WLI (145434), XA-FLI (145444), XA-JLI (145440), XA-KLI (145426), XA-XLI (145456), XA-RLI (145559), XA-ILI (145564), XA-ULI (145570), XA-VLI (145574), XA-SLI (145580), XA-QLI (145588), XA-TLI (145601), XA-ALI (145795), XA-BLI (145798), XA-CLI (14500803), XA-DLI (14500852), XA-ELI (14500861)

313102ALE 145

Rev. 1 June 19th, 2008 Page 2 de 6

Job Card

CLAVE:

F-GIN-23

NÚMERO DE REVISIÓN:

1

FECHA DE REVISIÓN:

10-MAR-08

Code:

RECORDING

Revision:

Indicating and Recording System

Revision Date:

INTERVALO:

H – H:

Interval:

Hrs-Men:

150 Hours

0.30

Removal and Installation of Auxiliary Flight Data Acquisition and Management Unit (AFDAMU) PCMCIA Card No. DE ORDEN DE INGENIERÍA:

No. DE TAREA: Task Number :

313102ALE 145

Enginnering Order Number:

N/A

ZONA:

PANEL DE ACCESO:

Zone:

Access Panel (s):

272

272DR

REQUERIDO POR: Required by:

AEROLITORAL

AD:

SB:

This task apply to: A/C Registration:______________

Aircraft

Date:

______________

P/N: ______________________ S/N: ______________________ Position:_____________

Component

2. Procedure (cont.)

DESCRIPTION

Tech. Cert. No. Signature

Insp. Stamp

G. AFDAMU PCMCIA Card – Install, see Figure No. 2 (a) Install the AFDAMU PCMCIA card (2) in the AFDAMU PCMCIA card slot (4), with the label facing the AFDAMU handle. NOTE: • When you insert the AFDAMU PCMCIA card to the AFDAMU PCMCIA card slot, the green color status LED blinks at a higher frequency (1 Hz approximately), as a manner of recognize the card during the loading procedure. The green color status LED stay ON after the loading procedure until the QAR is powered off • If the AFDAMU PCMCIA card is not full, the green color status LED will go out. • If the AFDAMU PCMCIA card is not correctly formatted, the amber color status LED comes on, close the AFDAMU PCMCIA unit access door and push to lock it. De-energize the aircraft (TASK 20-40-01-860-801-A) a minimum of 60 seconds, energize the aircraft with the External DC Power Supply (TASK 20-40-01-860 801-A), open the AFDAMU PCMCIA unit access door and verify the green color status LED, if the ambar color status LED still on, replace it with a new one. (b) Close the AFDAMU PCMCIA unit access door and push to lock it.

EFECTIVIDAD:

All EMB-145 Model

Effectivity

SERIAL A/C Registration (Serial Number)

XA-LLI (145060), XA-MLI (145065), XA-NLI (145083), XA-OLI (145089), XA-PLI (145090), XA-GLI (145203), XA-KAC (145322), XA-HLI (145337), XA-YLI (145400), XA-ZLI (145420), XA-WLI (145434), XA-FLI (145444), XA-JLI (145440), XA-KLI (145426), XA-XLI (145456), XA-RLI (145559), XA-ILI (145564), XA-ULI (145570), XA-VLI (145574), XA-SLI (145580), XA-QLI (145588), XA-TLI (145601), XA-ALI (145795), XA-BLI (145798), XA-CLI (14500803), XA-DLI (14500852), XA-ELI (14500861)

313102ALE 145

Rev. 1 June 19th, 2008 Page 3 de 6

Job Card

CLAVE:

F-GIN-23

NÚMERO DE REVISIÓN:

1

FECHA DE REVISIÓN:

10-MAR-08

Code:

RECORDING

Revision:

Indicating and Recording System

Revision Date:

INTERVALO:

H – H:

Interval:

Hrs-Men:

150 Hours

0.30

Removal and Installation of Auxiliary Flight Data Acquisition and Management Unit (AFDAMU) PCMCIA Card No. DE ORDEN DE INGENIERÍA:

No. DE TAREA: Task Number :

313102ALE 145

Enginnering Order Number:

N/A

ZONA:

PANEL DE ACCESO:

Zone:

Access Panel (s):

272

272DR

REQUERIDO POR: Required by:

AEROLITORAL

AD:

SB:

This task apply to: A/C Registration:______________

Aircraft

Date:

______________

P/N: ______________________ S/N: ______________________ Position:_____________

Component

2. Procedure (cont.)

DESCRIPTION

Tech. Cert. No. Signature

Insp. Stamp

H. Put a 2.5 inch of masking tape (MC083 or equivalent) to PCMCIA card removed and label it with A/C Registration and removal date. (example: XA-OLI 15-Mar-08) (a) Pack the PCMCIA card removed with the bag and carton box of new PCMCIA card installed and send it to the MTY warehouse. NOTE: Send a E-mail to Security Department (frojas@amconnect and jlugo@amconnect) to advise that one PCMCIA card was removed of A/C Registration. I. Close access door 272DR (AMM 06-41-01/101). J. Remove the hydraulic platform (GSE 036) or equivalent platform or Stair. K. Deenergize the aircraft (TASK 20-40-01-860-801-A). L. Enter the accomplishment of this Task 313102ALE 145 in the applicable document. - Record at the aircraft log book, the information of task(s) performed and its description as it is shown in the paragraph below. - Performed Task # 313102ALE 145, Description: Removal and Installation of Auxiliary Flight Data Acquisition and Management Unit (AFDAMU) PCMCIA Card. - Must fill the format RAMCO Technical Log (F-GIN-40). EFECTIVIDAD:

All EMB-145 Model

Effectivity

SERIAL A/C Registration (Serial Number)

XA-LLI (145060), XA-MLI (145065), XA-NLI (145083), XA-OLI (145089), XA-PLI (145090), XA-GLI (145203), XA-KAC (145322), XA-HLI (145337), XA-YLI (145400), XA-ZLI (145420), XA-WLI (145434), XA-FLI (145444), XA-JLI (145440), XA-KLI (145426), XA-XLI (145456), XA-RLI (145559), XA-ILI (145564), XA-ULI (145570), XA-VLI (145574), XA-SLI (145580), XA-QLI (145588), XA-TLI (145601), XA-ALI (145795), XA-BLI (145798), XA-CLI (14500803), XA-DLI (14500852), XA-ELI (14500861)

313102ALE 145

Rev. 1 June 19th, 2008 Page 4 de 6

Job Card

CLAVE:

F-GIN-23

NÚMERO DE REVISIÓN:

1

FECHA DE REVISIÓN:

10-MAR-08

Code:

RECORDING

Revision:

Indicating and Recording System

Revision Date:

INTERVALO:

H – H:

Interval:

Hrs-Men:

150 Hours

0.30

Removal and Installation of Auxiliary Flight Data Acquisition and Management Unit (AFDAMU) PCMCIA Card No. DE ORDEN DE INGENIERÍA:

No. DE TAREA: Task Number :

313102ALE 145

PANEL DE ACCESO:

Zone:

Access Panel (s):

272

272DR

REQUERIDO POR:

AEROLITORAL

Required by:

N/A

Enginnering Order Number:

ZONA:

AD:

SB:

:

COMM

MISCELLANEOUS

RMU 1

INTPH 1

VHF 1

AWS 1

FDR

FDAU

5

5

10

5

5

5

BAGGAGE FIRE PASS OXY EXTG DEPLOY 1

7½

10

PRESS CPAM

5

Figure No. 1: FDAU CIRCUIT BREAKER - Location (Sheet 01 of 01) EFECTIVIDAD:

All EMB-145 Model

Effectivity

SERIAL A/C Registration (Serial Number)

XA-LLI (145060), XA-MLI (145065), XA-NLI (145083), XA-OLI (145089), XA-PLI (145090), XA-GLI (145203), XA-KAC (145322), XA-HLI (145337), XA-YLI (145400), XA-ZLI (145420), XA-WLI (145434), XA-FLI (145444), XA-JLI (145440), XA-KLI (145426), XA-XLI (145456), XA-RLI (145559), XA-ILI (145564), XA-ULI (145570), XA-VLI (145574), XA-SLI (145580), XA-QLI (145588), XA-TLI (145601), XA-ALI (145795), XA-BLI (145798), XA-CLI (14500803), XA-DLI (14500852), XA-ELI (14500861)

313102ALE 145

Rev. 1 June 19th, 2008 Page 5 de 6

Job Card

CLAVE:

F-GIN-23

NÚMERO DE REVISIÓN:

1

FECHA DE REVISIÓN:

10-MAR-08

Code:

RECORDING

Revision:

Indicating and Recording System

Revision Date:

INTERVALO:

H – H:

Interval:

Hrs-Men:

150 Hours

0.30

No. DE ORDEN DE INGENIERÍA:

No. DE TAREA:

313102ALE 145

Task Number :

ZONA:

Removal and Installation of Auxiliary Flight Data Acquisition and Management Unit (AFDAMU) PCMCIA Card Enginnering Order Number:

PANEL DE ACCESO:

Zone:

Access Panel (s):

272

272DR

REQUERIDO POR:

AEROLITORAL

Required by:

N/A

AD:

SB:

DOOR 272DR

B

A ZONE 272

DET. A 1. AFDAMU

C

ON OFF

2. PCMCIA MEMORY CARD

DET. B 7. LOCK RELEASE SWITCH

6. FRONT PANEL DOOR

3. EJECT BUTTON

4. PCMCIA CARD SLOT

DET. C

5. PCMCIA OPERATION LEDS

Figure No. 2: AFDAMU PCMCIA CARD - Removal/Installation (Sheet 01 of 01) EFECTIVIDAD:

All EMB-145 Model

Effectivity

SERIAL A/C Registration (Serial Number)

XA-LLI (145060), XA-MLI (145065), XA-NLI (145083), XA-OLI (145089), XA-PLI (145090), XA-GLI (145203), XA-KAC (145322), XA-HLI (145337), XA-YLI (145400), XA-ZLI (145420), XA-WLI (145434), XA-FLI (145444), XA-JLI (145440), XA-KLI (145426), XA-XLI (145456), XA-RLI (145559), XA-ILI (145564), XA-ULI (145570), XA-VLI (145574), XA-SLI (145580), XA-QLI (145588), XA-TLI (145601), XA-ALI (145795), XA-BLI (145798), XA-CLI (14500803), XA-DLI (14500852), XA-ELI (14500861)

313102ALE 145

Rev. 1 June 19th, 2008 Page 6 de 6